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diff --git a/examples/scripts/ssbj/(X)DSM/RCG_basic.pdf b/examples/scripts/ssbj/(X)DSM/RCG_basic.pdf
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diff --git a/examples/scripts/ssbj/(X)DSM/RCG_extended.pdf b/examples/scripts/ssbj/(X)DSM/RCG_extended.pdf
index 9742bf36d13eb30739be318e0ea0e86cce20e7fa..2fda729d6f11f0f33b77cde19beca61e90bf3208 100644
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diff --git a/examples/scripts/ssbj/CMDOWS/FPG_MDA.xml b/examples/scripts/ssbj/CMDOWS/FPG_MDA.xml
index 31159a8f1f8b15122cb2e7af7893c868bfbda329..238396af5e0433ff4b98430ae445bdf206b7b07d 100644
--- a/examples/scripts/ssbj/CMDOWS/FPG_MDA.xml
+++ b/examples/scripts/ssbj/CMDOWS/FPG_MDA.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>FPG CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-21T15:55:30.252183</timestamp>
+    <timestamp>2018-03-24T09:14:31.749000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a fundamental problem graph (FPG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-21T15:55:30.252183</timestamp>
+        <timestamp>2018-03-24T09:14:31.749000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -532,16 +532,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
+              <sample position="1">0.100000000000</sample>
               <sample position="2">0.116666666667</sample>
               <sample position="3">0.133333333333</sample>
-              <sample position="4">0.15</sample>
+              <sample position="4">0.150000000000</sample>
               <sample position="5">0.166666666667</sample>
               <sample position="6">0.183333333333</sample>
-              <sample position="7">0.2</sample>
+              <sample position="7">0.200000000000</sample>
               <sample position="8">0.216666666667</sample>
               <sample position="9">0.233333333333</sample>
-              <sample position="10">0.25</sample>
+              <sample position="10">0.250000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/section">
@@ -554,7 +554,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -563,7 +563,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/other/Cf">
@@ -576,7 +576,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -585,7 +585,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/other/T">
@@ -598,16 +598,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
-              <sample position="2">0.15</sample>
-              <sample position="3">0.2</sample>
-              <sample position="4">0.25</sample>
-              <sample position="5">0.3</sample>
-              <sample position="6">0.35</sample>
-              <sample position="7">0.4</sample>
-              <sample position="8">0.45</sample>
-              <sample position="9">0.5</sample>
-              <sample position="10">0.55</sample>
+              <sample position="1">0.100000000000</sample>
+              <sample position="2">0.150000000000</sample>
+              <sample position="3">0.200000000000</sample>
+              <sample position="4">0.250000000000</sample>
+              <sample position="5">0.300000000000</sample>
+              <sample position="6">0.350000000000</sample>
+              <sample position="7">0.400000000000</sample>
+              <sample position="8">0.450000000000</sample>
+              <sample position="9">0.500000000000</sample>
+              <sample position="10">0.550000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/AR">
@@ -620,16 +620,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">2.5</sample>
-              <sample position="2">2.83333333333</sample>
-              <sample position="3">3.16666666667</sample>
-              <sample position="4">3.5</sample>
-              <sample position="5">3.83333333333</sample>
-              <sample position="6">4.16666666667</sample>
-              <sample position="7">4.5</sample>
-              <sample position="8">4.83333333333</sample>
-              <sample position="9">5.16666666667</sample>
-              <sample position="10">5.5</sample>
+              <sample position="1">2.500000000000</sample>
+              <sample position="2">2.833333333333</sample>
+              <sample position="3">3.166666666667</sample>
+              <sample position="4">3.500000000000</sample>
+              <sample position="5">3.833333333333</sample>
+              <sample position="6">4.166666666667</sample>
+              <sample position="7">4.500000000000</sample>
+              <sample position="8">4.833333333333</sample>
+              <sample position="9">5.166666666667</sample>
+              <sample position="10">5.500000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/Sref">
@@ -642,16 +642,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">500.0</sample>
-              <sample position="2">555.555555556</sample>
-              <sample position="3">611.111111111</sample>
-              <sample position="4">666.666666667</sample>
-              <sample position="5">722.222222222</sample>
-              <sample position="6">777.777777778</sample>
-              <sample position="7">833.333333333</sample>
-              <sample position="8">888.888888889</sample>
-              <sample position="9">944.444444444</sample>
-              <sample position="10">1000.0</sample>
+              <sample position="1">500.000000000000</sample>
+              <sample position="2">555.555555555556</sample>
+              <sample position="3">611.111111111111</sample>
+              <sample position="4">666.666666666667</sample>
+              <sample position="5">722.222222222222</sample>
+              <sample position="6">777.777777777778</sample>
+              <sample position="7">833.333333333333</sample>
+              <sample position="8">888.888888888889</sample>
+              <sample position="9">944.444444444444</sample>
+              <sample position="10">1000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/tc">
@@ -664,16 +664,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.01</sample>
-              <sample position="2">0.0144444444444</sample>
-              <sample position="3">0.0188888888889</sample>
-              <sample position="4">0.0233333333333</sample>
-              <sample position="5">0.0277777777778</sample>
-              <sample position="6">0.0322222222222</sample>
-              <sample position="7">0.0366666666667</sample>
-              <sample position="8">0.0411111111111</sample>
-              <sample position="9">0.0455555555556</sample>
-              <sample position="10">0.05</sample>
+              <sample position="1">0.010000000000</sample>
+              <sample position="2">0.014444444444</sample>
+              <sample position="3">0.018888888889</sample>
+              <sample position="4">0.023333333333</sample>
+              <sample position="5">0.027777777778</sample>
+              <sample position="6">0.032222222222</sample>
+              <sample position="7">0.036666666667</sample>
+              <sample position="8">0.041111111111</sample>
+              <sample position="9">0.045555555556</sample>
+              <sample position="10">0.050000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/h">
@@ -686,16 +686,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">30000.0</sample>
-              <sample position="2">31666.6666667</sample>
-              <sample position="3">33333.3333333</sample>
-              <sample position="4">35000.0</sample>
-              <sample position="5">36666.6666667</sample>
-              <sample position="6">38333.3333333</sample>
-              <sample position="7">40000.0</sample>
-              <sample position="8">41666.6666667</sample>
-              <sample position="9">43333.3333333</sample>
-              <sample position="10">45000.0</sample>
+              <sample position="1">30000.000000000000</sample>
+              <sample position="2">31666.666666666668</sample>
+              <sample position="3">33333.333333333336</sample>
+              <sample position="4">35000.000000000000</sample>
+              <sample position="5">36666.666666666664</sample>
+              <sample position="6">38333.333333333336</sample>
+              <sample position="7">40000.000000000000</sample>
+              <sample position="8">41666.666666666672</sample>
+              <sample position="9">43333.333333333336</sample>
+              <sample position="10">45000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/M">
@@ -708,16 +708,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">1.4</sample>
-              <sample position="2">1.42222222222</sample>
-              <sample position="3">1.44444444444</sample>
-              <sample position="4">1.46666666667</sample>
-              <sample position="5">1.48888888889</sample>
-              <sample position="6">1.51111111111</sample>
-              <sample position="7">1.53333333333</sample>
-              <sample position="8">1.55555555556</sample>
-              <sample position="9">1.57777777778</sample>
-              <sample position="10">1.6</sample>
+              <sample position="1">1.400000000000</sample>
+              <sample position="2">1.422222222222</sample>
+              <sample position="3">1.444444444444</sample>
+              <sample position="4">1.466666666667</sample>
+              <sample position="5">1.488888888889</sample>
+              <sample position="6">1.511111111111</sample>
+              <sample position="7">1.533333333333</sample>
+              <sample position="8">1.555555555556</sample>
+              <sample position="9">1.577777777778</sample>
+              <sample position="10">1.600000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/Lambda">
@@ -730,16 +730,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">40.0</sample>
-              <sample position="2">41.6666666667</sample>
-              <sample position="3">43.3333333333</sample>
-              <sample position="4">45.0</sample>
-              <sample position="5">46.6666666667</sample>
-              <sample position="6">48.3333333333</sample>
-              <sample position="7">50.0</sample>
-              <sample position="8">51.6666666667</sample>
-              <sample position="9">53.3333333333</sample>
-              <sample position="10">55.0</sample>
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+              <sample position="2">41.666666666667</sample>
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+              <sample position="6">48.333333333333</sample>
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+              <sample position="8">51.666666666667</sample>
+              <sample position="9">53.333333333333</sample>
+              <sample position="10">55.000000000000</sample>
             </samples>
           </designVariable>
         </designVariables>
diff --git a/examples/scripts/ssbj/CMDOWS/FPG_MDO.xml b/examples/scripts/ssbj/CMDOWS/FPG_MDO.xml
index 2c5ac488ca5da6e32a7a6d06c501922788a2011f..24ca928b26cd9ebd977de5155b10b6852d69d61c 100644
--- a/examples/scripts/ssbj/CMDOWS/FPG_MDO.xml
+++ b/examples/scripts/ssbj/CMDOWS/FPG_MDO.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>FPG CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-23T11:14:08.740222</timestamp>
+    <timestamp>2018-03-24T08:54:14.754000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a fundamental problem graph (FPG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-23T11:14:08.740222</timestamp>
+        <timestamp>2018-03-24T08:54:14.754000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_BLISS-2000.xml b/examples/scripts/ssbj/CMDOWS/Mdao_BLISS-2000.xml
index ef15fa9759a1a447d6d5671848013329f84bfdda..9809dc7a0c1d984f1b08626468f7c4a2e6a5953a 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_BLISS-2000.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_BLISS-2000.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-23T11:14:08.740222</timestamp>
+    <timestamp>2018-03-24T08:54:14.754000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-23T11:14:08.740222</timestamp>
+        <timestamp>2018-03-24T08:54:14.754000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -5222,7 +5222,7 @@
           <settings>
             <maximumIterations>1000</maximumIterations>
             <algorithm>Dakota Quasi-Newton method</algorithm>
-            <applyScaling>True</applyScaling>
+            <applyScaling>true</applyScaling>
             <maximumFunctionEvaluations>1000</maximumFunctionEvaluations>
             <constraintTolerance>0.0001</constraintTolerance>
             <convergenceTolerance>0.0001</convergenceTolerance>
@@ -5323,7 +5323,7 @@
           <settings>
             <maximumIterations>1000</maximumIterations>
             <algorithm>Dakota Quasi-Newton method</algorithm>
-            <applyScaling>True</applyScaling>
+            <applyScaling>true</applyScaling>
             <maximumFunctionEvaluations>1000</maximumFunctionEvaluations>
             <constraintTolerance>0.0001</constraintTolerance>
             <convergenceTolerance>0.0001</convergenceTolerance>
@@ -5367,7 +5367,7 @@
           <settings>
             <maximumIterations>1000</maximumIterations>
             <algorithm>Dakota Quasi-Newton method</algorithm>
-            <applyScaling>True</applyScaling>
+            <applyScaling>true</applyScaling>
             <maximumFunctionEvaluations>1000</maximumFunctionEvaluations>
             <constraintTolerance>0.0001</constraintTolerance>
             <convergenceTolerance>0.0001</convergenceTolerance>
@@ -5393,7 +5393,7 @@
           <settings>
             <maximumIterations>1000</maximumIterations>
             <algorithm>Dakota Quasi-Newton method</algorithm>
-            <applyScaling>True</applyScaling>
+            <applyScaling>true</applyScaling>
             <maximumFunctionEvaluations>1000</maximumFunctionEvaluations>
             <constraintTolerance>0.0001</constraintTolerance>
             <convergenceTolerance>0.0001</convergenceTolerance>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_CO.xml b/examples/scripts/ssbj/CMDOWS/Mdao_CO.xml
index 1c4e52d063525fbd1ae3296750686c425a7908d5..c3ad29f334fb3a6da1360d05d6bc881e7b1f4fb9 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_CO.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_CO.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-23T11:10:24.958091</timestamp>
+    <timestamp>2018-03-24T08:54:14.754000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-23T11:10:24.958091</timestamp>
+        <timestamp>2018-03-24T08:54:14.754000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -1907,15 +1907,15 @@
         </edge>
         <edge>
           <fromExecutableBlockUID>Sub-Optimizer-1</fromExecutableBlockUID>
-          <toParameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/reference/M</toParameterUID>
+          <toParameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/AR__i2</toParameterUID>
         </edge>
         <edge>
           <fromExecutableBlockUID>Sub-Optimizer-1</fromExecutableBlockUID>
-          <toParameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/AR__i2</toParameterUID>
+          <toParameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/Lambda__i2</toParameterUID>
         </edge>
         <edge>
           <fromExecutableBlockUID>Sub-Optimizer-1</fromExecutableBlockUID>
-          <toParameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/Lambda__i2</toParameterUID>
+          <toParameterUID>/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/reference/M</toParameterUID>
         </edge>
         <edge>
           <fromExecutableBlockUID>Sub-Optimizer-2</fromExecutableBlockUID>
@@ -3022,7 +3022,7 @@
           <settings>
             <maximumIterations>1000</maximumIterations>
             <algorithm>Dakota Quasi-Newton method</algorithm>
-            <applyScaling>True</applyScaling>
+            <applyScaling>true</applyScaling>
             <maximumFunctionEvaluations>1000</maximumFunctionEvaluations>
             <constraintTolerance>0.0001</constraintTolerance>
             <convergenceTolerance>0.0001</convergenceTolerance>
@@ -3096,7 +3096,7 @@
           <settings>
             <maximumIterations>1000</maximumIterations>
             <algorithm>Dakota Quasi-Newton method</algorithm>
-            <applyScaling>True</applyScaling>
+            <applyScaling>true</applyScaling>
             <maximumFunctionEvaluations>1000</maximumFunctionEvaluations>
             <constraintTolerance>0.0001</constraintTolerance>
             <convergenceTolerance>0.0001</convergenceTolerance>
@@ -3152,7 +3152,7 @@
           <settings>
             <maximumIterations>1000</maximumIterations>
             <algorithm>Dakota Quasi-Newton method</algorithm>
-            <applyScaling>True</applyScaling>
+            <applyScaling>true</applyScaling>
             <maximumFunctionEvaluations>1000</maximumFunctionEvaluations>
             <constraintTolerance>0.0001</constraintTolerance>
             <convergenceTolerance>0.0001</convergenceTolerance>
@@ -3196,7 +3196,7 @@
           <settings>
             <maximumIterations>1000</maximumIterations>
             <algorithm>Dakota Quasi-Newton method</algorithm>
-            <applyScaling>True</applyScaling>
+            <applyScaling>true</applyScaling>
             <maximumFunctionEvaluations>1000</maximumFunctionEvaluations>
             <constraintTolerance>0.0001</constraintTolerance>
             <convergenceTolerance>0.0001</convergenceTolerance>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_IDF.xml b/examples/scripts/ssbj/CMDOWS/Mdao_IDF.xml
index 90c1dd79d7eb72e442faa69fb9fdc610f87e2e2f..6ab3edd0907813b6e8366726dd1b5c8663d9a9f4 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_IDF.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_IDF.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-23T11:10:24.958091</timestamp>
+    <timestamp>2018-03-24T08:54:14.754000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-23T11:10:24.958091</timestamp>
+        <timestamp>2018-03-24T08:54:14.754000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -518,6 +518,9 @@
     </mathematicalFunctions>
   </executableBlocks>
   <parameters>
+    <parameter uID="/data_schema/mdo_data/constraints/dpdx">
+      <label>dpdx</label>
+    </parameter>
     <parameter uID="/data_schema/aircraft/other/dpdx">
       <label>dpdx</label>
     </parameter>
@@ -581,9 +584,6 @@
     <parameter uID="/data_schema/aircraft/geometry/lambda">
       <label>lambda</label>
     </parameter>
-    <parameter uID="/data_schema/mdo_data/constraints/dpdx">
-      <label>dpdx</label>
-    </parameter>
     <parameter uID="/data_schema/mdo_data/objectives/R">
       <label>R</label>
     </parameter>
@@ -801,11 +801,11 @@
           </objectiveVariable>
         </objectiveVariables>
         <constraintVariables>
-          <constraintVariable uID="__conVar__/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/geometry/gc_Theta">
-            <parameterUID>/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/geometry/gc_Theta</parameterUID>
-            <constraintType>equality</constraintType>
-            <constraintOperator>==</constraintOperator>
-            <referenceValue>0.0</referenceValue>
+          <constraintVariable uID="__conVar__/data_schema/mdo_data/constraints/dpdx">
+            <parameterUID>/data_schema/mdo_data/constraints/dpdx</parameterUID>
+            <constraintType>inequality</constraintType>
+            <constraintOperator>&lt;=</constraintOperator>
+            <referenceValue>1.04</referenceValue>
           </constraintVariable>
           <constraintVariable uID="__conVar__/data_schema/mdo_data/constraints/propulsion/ESF">
             <parameterUID>/data_schema/mdo_data/constraints/propulsion/ESF</parameterUID>
@@ -813,12 +813,6 @@
             <constraintOperator>&gt;=;&lt;=</constraintOperator>
             <referenceValue>0.5;1.5</referenceValue>
           </constraintVariable>
-          <constraintVariable uID="__conVar__/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/other/gc_L">
-            <parameterUID>/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/other/gc_L</parameterUID>
-            <constraintType>equality</constraintType>
-            <constraintOperator>==</constraintOperator>
-            <referenceValue>0.0</referenceValue>
-          </constraintVariable>
           <constraintVariable uID="__conVar__/data_schema/mdo_data/constraints/propulsion/DT">
             <parameterUID>/data_schema/mdo_data/constraints/propulsion/DT</parameterUID>
             <constraintType>inequality</constraintType>
@@ -837,6 +831,12 @@
             <constraintOperator>==</constraintOperator>
             <referenceValue>0.0</referenceValue>
           </constraintVariable>
+          <constraintVariable uID="__conVar__/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/geometry/gc_Theta">
+            <parameterUID>/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/geometry/gc_Theta</parameterUID>
+            <constraintType>equality</constraintType>
+            <constraintOperator>==</constraintOperator>
+            <referenceValue>0.0</referenceValue>
+          </constraintVariable>
           <constraintVariable uID="__conVar__/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/weight/gc_WT">
             <parameterUID>/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/weight/gc_WT</parameterUID>
             <constraintType>equality</constraintType>
@@ -849,18 +849,18 @@
             <constraintOperator>==</constraintOperator>
             <referenceValue>0.0</referenceValue>
           </constraintVariable>
+          <constraintVariable uID="__conVar__/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/other/gc_L">
+            <parameterUID>/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/other/gc_L</parameterUID>
+            <constraintType>equality</constraintType>
+            <constraintOperator>==</constraintOperator>
+            <referenceValue>0.0</referenceValue>
+          </constraintVariable>
           <constraintVariable uID="__conVar__/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/other/gc_D">
             <parameterUID>/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/other/gc_D</parameterUID>
             <constraintType>equality</constraintType>
             <constraintOperator>==</constraintOperator>
             <referenceValue>0.0</referenceValue>
           </constraintVariable>
-          <constraintVariable uID="__conVar__/data_schema/mdo_data/constraints/dpdx">
-            <parameterUID>/data_schema/mdo_data/constraints/dpdx</parameterUID>
-            <constraintType>inequality</constraintType>
-            <constraintOperator>&lt;=</constraintOperator>
-            <referenceValue>1.04</referenceValue>
-          </constraintVariable>
           <constraintVariable uID="__conVar__/data_schema/mdo_data/constraints/propulsion/Temp">
             <parameterUID>/data_schema/mdo_data/constraints/propulsion/Temp</parameterUID>
             <constraintType>inequality</constraintType>
@@ -939,7 +939,7 @@
           <toExecutableBlockUID>__Gc</toExecutableBlockUID>
         </edge>
         <edge>
-          <fromParameterUID>/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/geometry/gc_Theta</fromParameterUID>
+          <fromParameterUID>/data_schema/mdo_data/constraints/dpdx</fromParameterUID>
           <toExecutableBlockUID>Optimizer</toExecutableBlockUID>
         </edge>
         <edge>
@@ -1035,8 +1035,8 @@
           <toExecutableBlockUID>Optimizer</toExecutableBlockUID>
         </edge>
         <edge>
-          <fromParameterUID>/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/other/gc_L</fromParameterUID>
-          <toExecutableBlockUID>Optimizer</toExecutableBlockUID>
+          <fromParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/other/L</fromParameterUID>
+          <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
         </edge>
         <edge>
           <fromParameterUID>/data_schema/aircraft/other/D</fromParameterUID>
@@ -1322,6 +1322,10 @@
           <fromParameterUID>/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/dpdx</fromParameterUID>
           <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
         </edge>
+        <edge>
+          <fromParameterUID>/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/geometry/gc_Theta</fromParameterUID>
+          <toExecutableBlockUID>Optimizer</toExecutableBlockUID>
+        </edge>
         <edge>
           <fromParameterUID>/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/weight/gc_WT</fromParameterUID>
           <toExecutableBlockUID>Optimizer</toExecutableBlockUID>
@@ -1487,8 +1491,8 @@
           <toExecutableBlockUID>Optimizer</toExecutableBlockUID>
         </edge>
         <edge>
-          <fromParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/other/L</fromParameterUID>
-          <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
+          <fromParameterUID>/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/other/gc_L</fromParameterUID>
+          <toExecutableBlockUID>Optimizer</toExecutableBlockUID>
         </edge>
         <edge>
           <fromParameterUID>/data_schema/aircraft/geometry/lambda</fromParameterUID>
@@ -1510,10 +1514,6 @@
           <fromParameterUID>/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/reference/ESF</fromParameterUID>
           <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
         </edge>
-        <edge>
-          <fromParameterUID>/data_schema/mdo_data/constraints/dpdx</fromParameterUID>
-          <toExecutableBlockUID>Optimizer</toExecutableBlockUID>
-        </edge>
         <edge>
           <fromExecutableBlockUID>Performance[main][1][1.0]</fromExecutableBlockUID>
           <toParameterUID>/data_schema/aircraft/other/R</toParameterUID>
@@ -2026,6 +2026,10 @@
           <relatedParameterUID>/data_schema/aircraft/weight/WT</relatedParameterUID>
           <label>WT^{*}</label>
         </finalCouplingVariable>
+        <finalCouplingVariable uID="/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/other/L">
+          <relatedParameterUID>/data_schema/aircraft/other/L</relatedParameterUID>
+          <label>L^{*}</label>
+        </finalCouplingVariable>
         <finalCouplingVariable uID="/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/weight/WE">
           <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
           <label>WE^{*}</label>
@@ -2034,10 +2038,6 @@
           <relatedParameterUID>/data_schema/aircraft/other/D</relatedParameterUID>
           <label>D^{*}</label>
         </finalCouplingVariable>
-        <finalCouplingVariable uID="/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/aircraft/other/L">
-          <relatedParameterUID>/data_schema/aircraft/other/L</relatedParameterUID>
-          <label>L^{*}</label>
-        </finalCouplingVariable>
         <finalCouplingVariable uID="/data_schema/architectureNodes/finalCouplingVariables/data_schemaCopy/reference/ESF">
           <relatedParameterUID>/data_schema/reference/ESF</relatedParameterUID>
           <label>ESF^{*}</label>
@@ -2204,18 +2204,14 @@
         </finalOutputVariable>
       </finalOutputVariables>
       <consistencyConstraintVariables>
-        <consistencyConstraintVariable uID="/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/geometry/gc_Theta">
-          <relatedParameterUID>/data_schema/aircraft/geometry/Theta</relatedParameterUID>
-          <label>gc_Theta</label>
-        </consistencyConstraintVariable>
-        <consistencyConstraintVariable uID="/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/other/gc_L">
-          <relatedParameterUID>/data_schema/aircraft/other/L</relatedParameterUID>
-          <label>gc_L</label>
-        </consistencyConstraintVariable>
         <consistencyConstraintVariable uID="/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/weight/gc_WE">
           <relatedParameterUID>/data_schema/aircraft/weight/WE</relatedParameterUID>
           <label>gc_WE</label>
         </consistencyConstraintVariable>
+        <consistencyConstraintVariable uID="/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/geometry/gc_Theta">
+          <relatedParameterUID>/data_schema/aircraft/geometry/Theta</relatedParameterUID>
+          <label>gc_Theta</label>
+        </consistencyConstraintVariable>
         <consistencyConstraintVariable uID="/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/weight/gc_WT">
           <relatedParameterUID>/data_schema/aircraft/weight/WT</relatedParameterUID>
           <label>gc_WT</label>
@@ -2224,6 +2220,10 @@
           <relatedParameterUID>/data_schema/reference/ESF</relatedParameterUID>
           <label>gc_ESF</label>
         </consistencyConstraintVariable>
+        <consistencyConstraintVariable uID="/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/other/gc_L">
+          <relatedParameterUID>/data_schema/aircraft/other/L</relatedParameterUID>
+          <label>gc_L</label>
+        </consistencyConstraintVariable>
         <consistencyConstraintVariable uID="/data_schema/architectureNodes/consistencyConstraintVariables/data_schemaCopy/aircraft/other/gc_D">
           <relatedParameterUID>/data_schema/aircraft/other/D</relatedParameterUID>
           <label>gc_D</label>
@@ -2242,7 +2242,7 @@
           <settings>
             <maximumIterations>1000</maximumIterations>
             <algorithm>Dakota Quasi-Newton method</algorithm>
-            <applyScaling>True</applyScaling>
+            <applyScaling>true</applyScaling>
             <maximumFunctionEvaluations>1000</maximumFunctionEvaluations>
             <constraintTolerance>0.0001</constraintTolerance>
             <convergenceTolerance>0.0001</convergenceTolerance>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_MDF-GS.xml b/examples/scripts/ssbj/CMDOWS/Mdao_MDF-GS.xml
index 7694e39b3e32366c276845ce43ed8e3e3fa3871a..fa2e5f5f0f2e9c208b9ab3e8ba15b0d079e4e497 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_MDF-GS.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_MDF-GS.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-23T11:10:24.958091</timestamp>
+    <timestamp>2018-03-24T08:54:14.754000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-23T11:10:24.958091</timestamp>
+        <timestamp>2018-03-24T08:54:14.754000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -1857,7 +1857,7 @@
           <settings>
             <maximumIterations>1000</maximumIterations>
             <algorithm>Dakota Quasi-Newton method</algorithm>
-            <applyScaling>True</applyScaling>
+            <applyScaling>true</applyScaling>
             <maximumFunctionEvaluations>1000</maximumFunctionEvaluations>
             <constraintTolerance>0.0001</constraintTolerance>
             <convergenceTolerance>0.0001</convergenceTolerance>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_MDF-J.xml b/examples/scripts/ssbj/CMDOWS/Mdao_MDF-J.xml
index 85708f2443af67beb7602ffa9cc53e54458bcac5..e4ed2f1a0468943f16593c2d069958bb90a444c3 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_MDF-J.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_MDF-J.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-23T11:10:24.958091</timestamp>
+    <timestamp>2018-03-24T08:54:14.754000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-23T11:10:24.958091</timestamp>
+        <timestamp>2018-03-24T08:54:14.754000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -1984,7 +1984,7 @@
           <settings>
             <maximumIterations>1000</maximumIterations>
             <algorithm>Dakota Quasi-Newton method</algorithm>
-            <applyScaling>True</applyScaling>
+            <applyScaling>true</applyScaling>
             <maximumFunctionEvaluations>1000</maximumFunctionEvaluations>
             <constraintTolerance>0.0001</constraintTolerance>
             <convergenceTolerance>0.0001</convergenceTolerance>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-CT.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-CT.xml
index 2d2fe996d16b86550b57bf81e67102d455b29541..8eee279801c3ec843c9d01dd4bcd8d2e01b5db72 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-CT.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-CT.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-21T15:55:30.252183</timestamp>
+    <timestamp>2018-03-24T09:14:31.749000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-21T15:55:30.252183</timestamp>
+        <timestamp>2018-03-24T09:14:31.749000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -534,16 +534,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
-              <sample position="2">0.15</sample>
-              <sample position="3">0.2</sample>
-              <sample position="4">0.25</sample>
-              <sample position="5">0.3</sample>
-              <sample position="6">0.35</sample>
-              <sample position="7">0.4</sample>
-              <sample position="8">0.45</sample>
-              <sample position="9">0.5</sample>
-              <sample position="10">0.55</sample>
+              <sample position="1">0.100000000000</sample>
+              <sample position="2">0.150000000000</sample>
+              <sample position="3">0.200000000000</sample>
+              <sample position="4">0.250000000000</sample>
+              <sample position="5">0.300000000000</sample>
+              <sample position="6">0.350000000000</sample>
+              <sample position="7">0.400000000000</sample>
+              <sample position="8">0.450000000000</sample>
+              <sample position="9">0.500000000000</sample>
+              <sample position="10">0.550000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/other/Cf">
@@ -556,7 +556,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -565,7 +565,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/lambda">
@@ -578,16 +578,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
+              <sample position="1">0.100000000000</sample>
               <sample position="2">0.116666666667</sample>
               <sample position="3">0.133333333333</sample>
-              <sample position="4">0.15</sample>
+              <sample position="4">0.150000000000</sample>
               <sample position="5">0.166666666667</sample>
               <sample position="6">0.183333333333</sample>
-              <sample position="7">0.2</sample>
+              <sample position="7">0.200000000000</sample>
               <sample position="8">0.216666666667</sample>
               <sample position="9">0.233333333333</sample>
-              <sample position="10">0.25</sample>
+              <sample position="10">0.250000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/section">
@@ -600,7 +600,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -609,7 +609,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/AR">
@@ -622,16 +622,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">2.5</sample>
-              <sample position="2">2.83333333333</sample>
-              <sample position="3">3.16666666667</sample>
-              <sample position="4">3.5</sample>
-              <sample position="5">3.83333333333</sample>
-              <sample position="6">4.16666666667</sample>
-              <sample position="7">4.5</sample>
-              <sample position="8">4.83333333333</sample>
-              <sample position="9">5.16666666667</sample>
-              <sample position="10">5.5</sample>
+              <sample position="1">2.500000000000</sample>
+              <sample position="2">2.833333333333</sample>
+              <sample position="3">3.166666666667</sample>
+              <sample position="4">3.500000000000</sample>
+              <sample position="5">3.833333333333</sample>
+              <sample position="6">4.166666666667</sample>
+              <sample position="7">4.500000000000</sample>
+              <sample position="8">4.833333333333</sample>
+              <sample position="9">5.166666666667</sample>
+              <sample position="10">5.500000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/tc">
@@ -644,16 +644,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.01</sample>
-              <sample position="2">0.0144444444444</sample>
-              <sample position="3">0.0188888888889</sample>
-              <sample position="4">0.0233333333333</sample>
-              <sample position="5">0.0277777777778</sample>
-              <sample position="6">0.0322222222222</sample>
-              <sample position="7">0.0366666666667</sample>
-              <sample position="8">0.0411111111111</sample>
-              <sample position="9">0.0455555555556</sample>
-              <sample position="10">0.05</sample>
+              <sample position="1">0.010000000000</sample>
+              <sample position="2">0.014444444444</sample>
+              <sample position="3">0.018888888889</sample>
+              <sample position="4">0.023333333333</sample>
+              <sample position="5">0.027777777778</sample>
+              <sample position="6">0.032222222222</sample>
+              <sample position="7">0.036666666667</sample>
+              <sample position="8">0.041111111111</sample>
+              <sample position="9">0.045555555556</sample>
+              <sample position="10">0.050000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/Sref">
@@ -666,16 +666,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">500.0</sample>
-              <sample position="2">555.555555556</sample>
-              <sample position="3">611.111111111</sample>
-              <sample position="4">666.666666667</sample>
-              <sample position="5">722.222222222</sample>
-              <sample position="6">777.777777778</sample>
-              <sample position="7">833.333333333</sample>
-              <sample position="8">888.888888889</sample>
-              <sample position="9">944.444444444</sample>
-              <sample position="10">1000.0</sample>
+              <sample position="1">500.000000000000</sample>
+              <sample position="2">555.555555555556</sample>
+              <sample position="3">611.111111111111</sample>
+              <sample position="4">666.666666666667</sample>
+              <sample position="5">722.222222222222</sample>
+              <sample position="6">777.777777777778</sample>
+              <sample position="7">833.333333333333</sample>
+              <sample position="8">888.888888888889</sample>
+              <sample position="9">944.444444444444</sample>
+              <sample position="10">1000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/h">
@@ -688,16 +688,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">30000.0</sample>
-              <sample position="2">31666.6666667</sample>
-              <sample position="3">33333.3333333</sample>
-              <sample position="4">35000.0</sample>
-              <sample position="5">36666.6666667</sample>
-              <sample position="6">38333.3333333</sample>
-              <sample position="7">40000.0</sample>
-              <sample position="8">41666.6666667</sample>
-              <sample position="9">43333.3333333</sample>
-              <sample position="10">45000.0</sample>
+              <sample position="1">30000.000000000000</sample>
+              <sample position="2">31666.666666666668</sample>
+              <sample position="3">33333.333333333336</sample>
+              <sample position="4">35000.000000000000</sample>
+              <sample position="5">36666.666666666664</sample>
+              <sample position="6">38333.333333333336</sample>
+              <sample position="7">40000.000000000000</sample>
+              <sample position="8">41666.666666666672</sample>
+              <sample position="9">43333.333333333336</sample>
+              <sample position="10">45000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/M">
@@ -710,16 +710,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">1.4</sample>
-              <sample position="2">1.42222222222</sample>
-              <sample position="3">1.44444444444</sample>
-              <sample position="4">1.46666666667</sample>
-              <sample position="5">1.48888888889</sample>
-              <sample position="6">1.51111111111</sample>
-              <sample position="7">1.53333333333</sample>
-              <sample position="8">1.55555555556</sample>
-              <sample position="9">1.57777777778</sample>
-              <sample position="10">1.6</sample>
+              <sample position="1">1.400000000000</sample>
+              <sample position="2">1.422222222222</sample>
+              <sample position="3">1.444444444444</sample>
+              <sample position="4">1.466666666667</sample>
+              <sample position="5">1.488888888889</sample>
+              <sample position="6">1.511111111111</sample>
+              <sample position="7">1.533333333333</sample>
+              <sample position="8">1.555555555556</sample>
+              <sample position="9">1.577777777778</sample>
+              <sample position="10">1.600000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/Lambda">
@@ -732,16 +732,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">40.0</sample>
-              <sample position="2">41.6666666667</sample>
-              <sample position="3">43.3333333333</sample>
-              <sample position="4">45.0</sample>
-              <sample position="5">46.6666666667</sample>
-              <sample position="6">48.3333333333</sample>
-              <sample position="7">50.0</sample>
-              <sample position="8">51.6666666667</sample>
-              <sample position="9">53.3333333333</sample>
-              <sample position="10">55.0</sample>
+              <sample position="1">40.000000000000</sample>
+              <sample position="2">41.666666666667</sample>
+              <sample position="3">43.333333333333</sample>
+              <sample position="4">45.000000000000</sample>
+              <sample position="5">46.666666666667</sample>
+              <sample position="6">48.333333333333</sample>
+              <sample position="7">50.000000000000</sample>
+              <sample position="8">51.666666666667</sample>
+              <sample position="9">53.333333333333</sample>
+              <sample position="10">55.000000000000</sample>
             </samples>
           </designVariable>
         </designVariables>
@@ -1783,19 +1783,19 @@
             <doeMethod>Custom design table</doeMethod>
             <doeTable>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/lambda">
-                <tableElement experimentID="0">0.1</tableElement>
+                <tableElement experimentID="0">0.100000000000</tableElement>
                 <tableElement experimentID="1">0.116666666667</tableElement>
                 <tableElement experimentID="2">0.133333333333</tableElement>
-                <tableElement experimentID="3">0.15</tableElement>
+                <tableElement experimentID="3">0.150000000000</tableElement>
                 <tableElement experimentID="4">0.166666666667</tableElement>
                 <tableElement experimentID="5">0.183333333333</tableElement>
-                <tableElement experimentID="6">0.2</tableElement>
+                <tableElement experimentID="6">0.200000000000</tableElement>
                 <tableElement experimentID="7">0.216666666667</tableElement>
                 <tableElement experimentID="8">0.233333333333</tableElement>
-                <tableElement experimentID="9">0.25</tableElement>
+                <tableElement experimentID="9">0.250000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/section">
-                <tableElement experimentID="0">0.75</tableElement>
+                <tableElement experimentID="0">0.750000000000</tableElement>
                 <tableElement experimentID="1">0.777777777778</tableElement>
                 <tableElement experimentID="2">0.805555555556</tableElement>
                 <tableElement experimentID="3">0.833333333333</tableElement>
@@ -1804,10 +1804,10 @@
                 <tableElement experimentID="6">0.916666666667</tableElement>
                 <tableElement experimentID="7">0.944444444444</tableElement>
                 <tableElement experimentID="8">0.972222222222</tableElement>
-                <tableElement experimentID="9">1.0</tableElement>
+                <tableElement experimentID="9">1.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/other/Cf">
-                <tableElement experimentID="0">0.75</tableElement>
+                <tableElement experimentID="0">0.750000000000</tableElement>
                 <tableElement experimentID="1">0.777777777778</tableElement>
                 <tableElement experimentID="2">0.805555555556</tableElement>
                 <tableElement experimentID="3">0.833333333333</tableElement>
@@ -1816,91 +1816,91 @@
                 <tableElement experimentID="6">0.916666666667</tableElement>
                 <tableElement experimentID="7">0.944444444444</tableElement>
                 <tableElement experimentID="8">0.972222222222</tableElement>
-                <tableElement experimentID="9">1.0</tableElement>
+                <tableElement experimentID="9">1.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/other/T">
-                <tableElement experimentID="0">0.1</tableElement>
-                <tableElement experimentID="1">0.15</tableElement>
-                <tableElement experimentID="2">0.2</tableElement>
-                <tableElement experimentID="3">0.25</tableElement>
-                <tableElement experimentID="4">0.3</tableElement>
-                <tableElement experimentID="5">0.35</tableElement>
-                <tableElement experimentID="6">0.4</tableElement>
-                <tableElement experimentID="7">0.45</tableElement>
-                <tableElement experimentID="8">0.5</tableElement>
-                <tableElement experimentID="9">0.55</tableElement>
+                <tableElement experimentID="0">0.100000000000</tableElement>
+                <tableElement experimentID="1">0.150000000000</tableElement>
+                <tableElement experimentID="2">0.200000000000</tableElement>
+                <tableElement experimentID="3">0.250000000000</tableElement>
+                <tableElement experimentID="4">0.300000000000</tableElement>
+                <tableElement experimentID="5">0.350000000000</tableElement>
+                <tableElement experimentID="6">0.400000000000</tableElement>
+                <tableElement experimentID="7">0.450000000000</tableElement>
+                <tableElement experimentID="8">0.500000000000</tableElement>
+                <tableElement experimentID="9">0.550000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/AR">
-                <tableElement experimentID="0">2.5</tableElement>
-                <tableElement experimentID="1">2.83333333333</tableElement>
-                <tableElement experimentID="2">3.16666666667</tableElement>
-                <tableElement experimentID="3">3.5</tableElement>
-                <tableElement experimentID="4">3.83333333333</tableElement>
-                <tableElement experimentID="5">4.16666666667</tableElement>
-                <tableElement experimentID="6">4.5</tableElement>
-                <tableElement experimentID="7">4.83333333333</tableElement>
-                <tableElement experimentID="8">5.16666666667</tableElement>
-                <tableElement experimentID="9">5.5</tableElement>
+                <tableElement experimentID="0">2.500000000000</tableElement>
+                <tableElement experimentID="1">2.833333333333</tableElement>
+                <tableElement experimentID="2">3.166666666667</tableElement>
+                <tableElement experimentID="3">3.500000000000</tableElement>
+                <tableElement experimentID="4">3.833333333333</tableElement>
+                <tableElement experimentID="5">4.166666666667</tableElement>
+                <tableElement experimentID="6">4.500000000000</tableElement>
+                <tableElement experimentID="7">4.833333333333</tableElement>
+                <tableElement experimentID="8">5.166666666667</tableElement>
+                <tableElement experimentID="9">5.500000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/Lambda">
-                <tableElement experimentID="0">40.0</tableElement>
-                <tableElement experimentID="1">41.6666666667</tableElement>
-                <tableElement experimentID="2">43.3333333333</tableElement>
-                <tableElement experimentID="3">45.0</tableElement>
-                <tableElement experimentID="4">46.6666666667</tableElement>
-                <tableElement experimentID="5">48.3333333333</tableElement>
-                <tableElement experimentID="6">50.0</tableElement>
-                <tableElement experimentID="7">51.6666666667</tableElement>
-                <tableElement experimentID="8">53.3333333333</tableElement>
-                <tableElement experimentID="9">55.0</tableElement>
+                <tableElement experimentID="0">40.000000000000</tableElement>
+                <tableElement experimentID="1">41.666666666667</tableElement>
+                <tableElement experimentID="2">43.333333333333</tableElement>
+                <tableElement experimentID="3">45.000000000000</tableElement>
+                <tableElement experimentID="4">46.666666666667</tableElement>
+                <tableElement experimentID="5">48.333333333333</tableElement>
+                <tableElement experimentID="6">50.000000000000</tableElement>
+                <tableElement experimentID="7">51.666666666667</tableElement>
+                <tableElement experimentID="8">53.333333333333</tableElement>
+                <tableElement experimentID="9">55.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/Sref">
-                <tableElement experimentID="0">500.0</tableElement>
-                <tableElement experimentID="1">555.555555556</tableElement>
-                <tableElement experimentID="2">611.111111111</tableElement>
-                <tableElement experimentID="3">666.666666667</tableElement>
-                <tableElement experimentID="4">722.222222222</tableElement>
-                <tableElement experimentID="5">777.777777778</tableElement>
-                <tableElement experimentID="6">833.333333333</tableElement>
-                <tableElement experimentID="7">888.888888889</tableElement>
-                <tableElement experimentID="8">944.444444444</tableElement>
-                <tableElement experimentID="9">1000.0</tableElement>
+                <tableElement experimentID="0">500.000000000000</tableElement>
+                <tableElement experimentID="1">555.555555555556</tableElement>
+                <tableElement experimentID="2">611.111111111111</tableElement>
+                <tableElement experimentID="3">666.666666666667</tableElement>
+                <tableElement experimentID="4">722.222222222222</tableElement>
+                <tableElement experimentID="5">777.777777777778</tableElement>
+                <tableElement experimentID="6">833.333333333333</tableElement>
+                <tableElement experimentID="7">888.888888888889</tableElement>
+                <tableElement experimentID="8">944.444444444444</tableElement>
+                <tableElement experimentID="9">1000.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/tc">
-                <tableElement experimentID="0">0.01</tableElement>
-                <tableElement experimentID="1">0.0144444444444</tableElement>
-                <tableElement experimentID="2">0.0188888888889</tableElement>
-                <tableElement experimentID="3">0.0233333333333</tableElement>
-                <tableElement experimentID="4">0.0277777777778</tableElement>
-                <tableElement experimentID="5">0.0322222222222</tableElement>
-                <tableElement experimentID="6">0.0366666666667</tableElement>
-                <tableElement experimentID="7">0.0411111111111</tableElement>
-                <tableElement experimentID="8">0.0455555555556</tableElement>
-                <tableElement experimentID="9">0.05</tableElement>
+                <tableElement experimentID="0">0.010000000000</tableElement>
+                <tableElement experimentID="1">0.014444444444</tableElement>
+                <tableElement experimentID="2">0.018888888889</tableElement>
+                <tableElement experimentID="3">0.023333333333</tableElement>
+                <tableElement experimentID="4">0.027777777778</tableElement>
+                <tableElement experimentID="5">0.032222222222</tableElement>
+                <tableElement experimentID="6">0.036666666667</tableElement>
+                <tableElement experimentID="7">0.041111111111</tableElement>
+                <tableElement experimentID="8">0.045555555556</tableElement>
+                <tableElement experimentID="9">0.050000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/reference/h">
-                <tableElement experimentID="0">30000.0</tableElement>
-                <tableElement experimentID="1">31666.6666667</tableElement>
-                <tableElement experimentID="2">33333.3333333</tableElement>
-                <tableElement experimentID="3">35000.0</tableElement>
-                <tableElement experimentID="4">36666.6666667</tableElement>
-                <tableElement experimentID="5">38333.3333333</tableElement>
-                <tableElement experimentID="6">40000.0</tableElement>
-                <tableElement experimentID="7">41666.6666667</tableElement>
-                <tableElement experimentID="8">43333.3333333</tableElement>
-                <tableElement experimentID="9">45000.0</tableElement>
+                <tableElement experimentID="0">30000.000000000000</tableElement>
+                <tableElement experimentID="1">31666.666666666668</tableElement>
+                <tableElement experimentID="2">33333.333333333336</tableElement>
+                <tableElement experimentID="3">35000.000000000000</tableElement>
+                <tableElement experimentID="4">36666.666666666664</tableElement>
+                <tableElement experimentID="5">38333.333333333336</tableElement>
+                <tableElement experimentID="6">40000.000000000000</tableElement>
+                <tableElement experimentID="7">41666.666666666672</tableElement>
+                <tableElement experimentID="8">43333.333333333336</tableElement>
+                <tableElement experimentID="9">45000.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/reference/M">
-                <tableElement experimentID="0">1.4</tableElement>
-                <tableElement experimentID="1">1.42222222222</tableElement>
-                <tableElement experimentID="2">1.44444444444</tableElement>
-                <tableElement experimentID="3">1.46666666667</tableElement>
-                <tableElement experimentID="4">1.48888888889</tableElement>
-                <tableElement experimentID="5">1.51111111111</tableElement>
-                <tableElement experimentID="6">1.53333333333</tableElement>
-                <tableElement experimentID="7">1.55555555556</tableElement>
-                <tableElement experimentID="8">1.57777777778</tableElement>
-                <tableElement experimentID="9">1.6</tableElement>
+                <tableElement experimentID="0">1.400000000000</tableElement>
+                <tableElement experimentID="1">1.422222222222</tableElement>
+                <tableElement experimentID="2">1.444444444444</tableElement>
+                <tableElement experimentID="3">1.466666666667</tableElement>
+                <tableElement experimentID="4">1.488888888889</tableElement>
+                <tableElement experimentID="5">1.511111111111</tableElement>
+                <tableElement experimentID="6">1.533333333333</tableElement>
+                <tableElement experimentID="7">1.555555555556</tableElement>
+                <tableElement experimentID="8">1.577777777778</tableElement>
+                <tableElement experimentID="9">1.600000000000</tableElement>
               </tableRow>
             </doeTable>
           </settings>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-FF.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-FF.xml
index fa391d6b91236f12a21f5862b060d054e019f270..d0c482ac37f85a14430a1730793e927439bea8d9 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-FF.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-FF.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-21T15:55:30.252183</timestamp>
+    <timestamp>2018-03-24T09:14:31.749000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-21T15:55:30.252183</timestamp>
+        <timestamp>2018-03-24T09:14:31.749000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -535,16 +535,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
-              <sample position="2">0.15</sample>
-              <sample position="3">0.2</sample>
-              <sample position="4">0.25</sample>
-              <sample position="5">0.3</sample>
-              <sample position="6">0.35</sample>
-              <sample position="7">0.4</sample>
-              <sample position="8">0.45</sample>
-              <sample position="9">0.5</sample>
-              <sample position="10">0.55</sample>
+              <sample position="1">0.100000000000</sample>
+              <sample position="2">0.150000000000</sample>
+              <sample position="3">0.200000000000</sample>
+              <sample position="4">0.250000000000</sample>
+              <sample position="5">0.300000000000</sample>
+              <sample position="6">0.350000000000</sample>
+              <sample position="7">0.400000000000</sample>
+              <sample position="8">0.450000000000</sample>
+              <sample position="9">0.500000000000</sample>
+              <sample position="10">0.550000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/other/Cf">
@@ -557,7 +557,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -566,7 +566,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/lambda">
@@ -579,16 +579,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
+              <sample position="1">0.100000000000</sample>
               <sample position="2">0.116666666667</sample>
               <sample position="3">0.133333333333</sample>
-              <sample position="4">0.15</sample>
+              <sample position="4">0.150000000000</sample>
               <sample position="5">0.166666666667</sample>
               <sample position="6">0.183333333333</sample>
-              <sample position="7">0.2</sample>
+              <sample position="7">0.200000000000</sample>
               <sample position="8">0.216666666667</sample>
               <sample position="9">0.233333333333</sample>
-              <sample position="10">0.25</sample>
+              <sample position="10">0.250000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/section">
@@ -601,7 +601,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -610,7 +610,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/AR">
@@ -623,16 +623,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">2.5</sample>
-              <sample position="2">2.83333333333</sample>
-              <sample position="3">3.16666666667</sample>
-              <sample position="4">3.5</sample>
-              <sample position="5">3.83333333333</sample>
-              <sample position="6">4.16666666667</sample>
-              <sample position="7">4.5</sample>
-              <sample position="8">4.83333333333</sample>
-              <sample position="9">5.16666666667</sample>
-              <sample position="10">5.5</sample>
+              <sample position="1">2.500000000000</sample>
+              <sample position="2">2.833333333333</sample>
+              <sample position="3">3.166666666667</sample>
+              <sample position="4">3.500000000000</sample>
+              <sample position="5">3.833333333333</sample>
+              <sample position="6">4.166666666667</sample>
+              <sample position="7">4.500000000000</sample>
+              <sample position="8">4.833333333333</sample>
+              <sample position="9">5.166666666667</sample>
+              <sample position="10">5.500000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/tc">
@@ -645,16 +645,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.01</sample>
-              <sample position="2">0.0144444444444</sample>
-              <sample position="3">0.0188888888889</sample>
-              <sample position="4">0.0233333333333</sample>
-              <sample position="5">0.0277777777778</sample>
-              <sample position="6">0.0322222222222</sample>
-              <sample position="7">0.0366666666667</sample>
-              <sample position="8">0.0411111111111</sample>
-              <sample position="9">0.0455555555556</sample>
-              <sample position="10">0.05</sample>
+              <sample position="1">0.010000000000</sample>
+              <sample position="2">0.014444444444</sample>
+              <sample position="3">0.018888888889</sample>
+              <sample position="4">0.023333333333</sample>
+              <sample position="5">0.027777777778</sample>
+              <sample position="6">0.032222222222</sample>
+              <sample position="7">0.036666666667</sample>
+              <sample position="8">0.041111111111</sample>
+              <sample position="9">0.045555555556</sample>
+              <sample position="10">0.050000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/Sref">
@@ -667,16 +667,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">500.0</sample>
-              <sample position="2">555.555555556</sample>
-              <sample position="3">611.111111111</sample>
-              <sample position="4">666.666666667</sample>
-              <sample position="5">722.222222222</sample>
-              <sample position="6">777.777777778</sample>
-              <sample position="7">833.333333333</sample>
-              <sample position="8">888.888888889</sample>
-              <sample position="9">944.444444444</sample>
-              <sample position="10">1000.0</sample>
+              <sample position="1">500.000000000000</sample>
+              <sample position="2">555.555555555556</sample>
+              <sample position="3">611.111111111111</sample>
+              <sample position="4">666.666666666667</sample>
+              <sample position="5">722.222222222222</sample>
+              <sample position="6">777.777777777778</sample>
+              <sample position="7">833.333333333333</sample>
+              <sample position="8">888.888888888889</sample>
+              <sample position="9">944.444444444444</sample>
+              <sample position="10">1000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/h">
@@ -689,16 +689,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">30000.0</sample>
-              <sample position="2">31666.6666667</sample>
-              <sample position="3">33333.3333333</sample>
-              <sample position="4">35000.0</sample>
-              <sample position="5">36666.6666667</sample>
-              <sample position="6">38333.3333333</sample>
-              <sample position="7">40000.0</sample>
-              <sample position="8">41666.6666667</sample>
-              <sample position="9">43333.3333333</sample>
-              <sample position="10">45000.0</sample>
+              <sample position="1">30000.000000000000</sample>
+              <sample position="2">31666.666666666668</sample>
+              <sample position="3">33333.333333333336</sample>
+              <sample position="4">35000.000000000000</sample>
+              <sample position="5">36666.666666666664</sample>
+              <sample position="6">38333.333333333336</sample>
+              <sample position="7">40000.000000000000</sample>
+              <sample position="8">41666.666666666672</sample>
+              <sample position="9">43333.333333333336</sample>
+              <sample position="10">45000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/M">
@@ -711,16 +711,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">1.4</sample>
-              <sample position="2">1.42222222222</sample>
-              <sample position="3">1.44444444444</sample>
-              <sample position="4">1.46666666667</sample>
-              <sample position="5">1.48888888889</sample>
-              <sample position="6">1.51111111111</sample>
-              <sample position="7">1.53333333333</sample>
-              <sample position="8">1.55555555556</sample>
-              <sample position="9">1.57777777778</sample>
-              <sample position="10">1.6</sample>
+              <sample position="1">1.400000000000</sample>
+              <sample position="2">1.422222222222</sample>
+              <sample position="3">1.444444444444</sample>
+              <sample position="4">1.466666666667</sample>
+              <sample position="5">1.488888888889</sample>
+              <sample position="6">1.511111111111</sample>
+              <sample position="7">1.533333333333</sample>
+              <sample position="8">1.555555555556</sample>
+              <sample position="9">1.577777777778</sample>
+              <sample position="10">1.600000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/Lambda">
@@ -733,16 +733,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">40.0</sample>
-              <sample position="2">41.6666666667</sample>
-              <sample position="3">43.3333333333</sample>
-              <sample position="4">45.0</sample>
-              <sample position="5">46.6666666667</sample>
-              <sample position="6">48.3333333333</sample>
-              <sample position="7">50.0</sample>
-              <sample position="8">51.6666666667</sample>
-              <sample position="9">53.3333333333</sample>
-              <sample position="10">55.0</sample>
+              <sample position="1">40.000000000000</sample>
+              <sample position="2">41.666666666667</sample>
+              <sample position="3">43.333333333333</sample>
+              <sample position="4">45.000000000000</sample>
+              <sample position="5">46.666666666667</sample>
+              <sample position="6">48.333333333333</sample>
+              <sample position="7">50.000000000000</sample>
+              <sample position="8">51.666666666667</sample>
+              <sample position="9">53.333333333333</sample>
+              <sample position="10">55.000000000000</sample>
             </samples>
           </designVariable>
         </designVariables>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-LH.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-LH.xml
index 42dbfb2c7795e974f50a4a773b11637d0f8b768a..bffc442991c0019685d1da4c95e5e0c0ff502493 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-LH.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-LH.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-21T15:55:30.252183</timestamp>
+    <timestamp>2018-03-24T09:14:31.749000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-21T15:55:30.252183</timestamp>
+        <timestamp>2018-03-24T09:14:31.749000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -535,16 +535,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
-              <sample position="2">0.15</sample>
-              <sample position="3">0.2</sample>
-              <sample position="4">0.25</sample>
-              <sample position="5">0.3</sample>
-              <sample position="6">0.35</sample>
-              <sample position="7">0.4</sample>
-              <sample position="8">0.45</sample>
-              <sample position="9">0.5</sample>
-              <sample position="10">0.55</sample>
+              <sample position="1">0.100000000000</sample>
+              <sample position="2">0.150000000000</sample>
+              <sample position="3">0.200000000000</sample>
+              <sample position="4">0.250000000000</sample>
+              <sample position="5">0.300000000000</sample>
+              <sample position="6">0.350000000000</sample>
+              <sample position="7">0.400000000000</sample>
+              <sample position="8">0.450000000000</sample>
+              <sample position="9">0.500000000000</sample>
+              <sample position="10">0.550000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/other/Cf">
@@ -557,7 +557,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -566,7 +566,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/lambda">
@@ -579,16 +579,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
+              <sample position="1">0.100000000000</sample>
               <sample position="2">0.116666666667</sample>
               <sample position="3">0.133333333333</sample>
-              <sample position="4">0.15</sample>
+              <sample position="4">0.150000000000</sample>
               <sample position="5">0.166666666667</sample>
               <sample position="6">0.183333333333</sample>
-              <sample position="7">0.2</sample>
+              <sample position="7">0.200000000000</sample>
               <sample position="8">0.216666666667</sample>
               <sample position="9">0.233333333333</sample>
-              <sample position="10">0.25</sample>
+              <sample position="10">0.250000000000</sample>
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           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/section">
@@ -601,7 +601,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -610,7 +610,7 @@
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               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
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+              <sample position="10">1.000000000000</sample>
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           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/AR">
@@ -623,16 +623,16 @@
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@@ -645,16 +645,16 @@
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@@ -667,16 +667,16 @@
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@@ -689,16 +689,16 @@
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@@ -711,16 +711,16 @@
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@@ -733,16 +733,16 @@
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-              <sample position="10">55.0</sample>
+              <sample position="1">40.000000000000</sample>
+              <sample position="2">41.666666666667</sample>
+              <sample position="3">43.333333333333</sample>
+              <sample position="4">45.000000000000</sample>
+              <sample position="5">46.666666666667</sample>
+              <sample position="6">48.333333333333</sample>
+              <sample position="7">50.000000000000</sample>
+              <sample position="8">51.666666666667</sample>
+              <sample position="9">53.333333333333</sample>
+              <sample position="10">55.000000000000</sample>
             </samples>
           </designVariable>
         </designVariables>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-MC.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-MC.xml
index 3df994ef927e63b197afae010c2de4789f9e8451..13942e391508872136c8679b199fda4c0b10f8c1 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-MC.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-GS-MC.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-21T15:55:30.252183</timestamp>
+    <timestamp>2018-03-24T09:14:31.749000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-21T15:55:30.252183</timestamp>
+        <timestamp>2018-03-24T09:14:31.749000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -535,16 +535,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
-              <sample position="2">0.15</sample>
-              <sample position="3">0.2</sample>
-              <sample position="4">0.25</sample>
-              <sample position="5">0.3</sample>
-              <sample position="6">0.35</sample>
-              <sample position="7">0.4</sample>
-              <sample position="8">0.45</sample>
-              <sample position="9">0.5</sample>
-              <sample position="10">0.55</sample>
+              <sample position="1">0.100000000000</sample>
+              <sample position="2">0.150000000000</sample>
+              <sample position="3">0.200000000000</sample>
+              <sample position="4">0.250000000000</sample>
+              <sample position="5">0.300000000000</sample>
+              <sample position="6">0.350000000000</sample>
+              <sample position="7">0.400000000000</sample>
+              <sample position="8">0.450000000000</sample>
+              <sample position="9">0.500000000000</sample>
+              <sample position="10">0.550000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/other/Cf">
@@ -557,7 +557,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -566,7 +566,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/lambda">
@@ -579,16 +579,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
+              <sample position="1">0.100000000000</sample>
               <sample position="2">0.116666666667</sample>
               <sample position="3">0.133333333333</sample>
-              <sample position="4">0.15</sample>
+              <sample position="4">0.150000000000</sample>
               <sample position="5">0.166666666667</sample>
               <sample position="6">0.183333333333</sample>
-              <sample position="7">0.2</sample>
+              <sample position="7">0.200000000000</sample>
               <sample position="8">0.216666666667</sample>
               <sample position="9">0.233333333333</sample>
-              <sample position="10">0.25</sample>
+              <sample position="10">0.250000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/section">
@@ -601,7 +601,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -610,7 +610,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/AR">
@@ -623,16 +623,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">2.5</sample>
-              <sample position="2">2.83333333333</sample>
-              <sample position="3">3.16666666667</sample>
-              <sample position="4">3.5</sample>
-              <sample position="5">3.83333333333</sample>
-              <sample position="6">4.16666666667</sample>
-              <sample position="7">4.5</sample>
-              <sample position="8">4.83333333333</sample>
-              <sample position="9">5.16666666667</sample>
-              <sample position="10">5.5</sample>
+              <sample position="1">2.500000000000</sample>
+              <sample position="2">2.833333333333</sample>
+              <sample position="3">3.166666666667</sample>
+              <sample position="4">3.500000000000</sample>
+              <sample position="5">3.833333333333</sample>
+              <sample position="6">4.166666666667</sample>
+              <sample position="7">4.500000000000</sample>
+              <sample position="8">4.833333333333</sample>
+              <sample position="9">5.166666666667</sample>
+              <sample position="10">5.500000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/tc">
@@ -645,16 +645,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.01</sample>
-              <sample position="2">0.0144444444444</sample>
-              <sample position="3">0.0188888888889</sample>
-              <sample position="4">0.0233333333333</sample>
-              <sample position="5">0.0277777777778</sample>
-              <sample position="6">0.0322222222222</sample>
-              <sample position="7">0.0366666666667</sample>
-              <sample position="8">0.0411111111111</sample>
-              <sample position="9">0.0455555555556</sample>
-              <sample position="10">0.05</sample>
+              <sample position="1">0.010000000000</sample>
+              <sample position="2">0.014444444444</sample>
+              <sample position="3">0.018888888889</sample>
+              <sample position="4">0.023333333333</sample>
+              <sample position="5">0.027777777778</sample>
+              <sample position="6">0.032222222222</sample>
+              <sample position="7">0.036666666667</sample>
+              <sample position="8">0.041111111111</sample>
+              <sample position="9">0.045555555556</sample>
+              <sample position="10">0.050000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/Sref">
@@ -667,16 +667,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">500.0</sample>
-              <sample position="2">555.555555556</sample>
-              <sample position="3">611.111111111</sample>
-              <sample position="4">666.666666667</sample>
-              <sample position="5">722.222222222</sample>
-              <sample position="6">777.777777778</sample>
-              <sample position="7">833.333333333</sample>
-              <sample position="8">888.888888889</sample>
-              <sample position="9">944.444444444</sample>
-              <sample position="10">1000.0</sample>
+              <sample position="1">500.000000000000</sample>
+              <sample position="2">555.555555555556</sample>
+              <sample position="3">611.111111111111</sample>
+              <sample position="4">666.666666666667</sample>
+              <sample position="5">722.222222222222</sample>
+              <sample position="6">777.777777777778</sample>
+              <sample position="7">833.333333333333</sample>
+              <sample position="8">888.888888888889</sample>
+              <sample position="9">944.444444444444</sample>
+              <sample position="10">1000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/h">
@@ -689,16 +689,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">30000.0</sample>
-              <sample position="2">31666.6666667</sample>
-              <sample position="3">33333.3333333</sample>
-              <sample position="4">35000.0</sample>
-              <sample position="5">36666.6666667</sample>
-              <sample position="6">38333.3333333</sample>
-              <sample position="7">40000.0</sample>
-              <sample position="8">41666.6666667</sample>
-              <sample position="9">43333.3333333</sample>
-              <sample position="10">45000.0</sample>
+              <sample position="1">30000.000000000000</sample>
+              <sample position="2">31666.666666666668</sample>
+              <sample position="3">33333.333333333336</sample>
+              <sample position="4">35000.000000000000</sample>
+              <sample position="5">36666.666666666664</sample>
+              <sample position="6">38333.333333333336</sample>
+              <sample position="7">40000.000000000000</sample>
+              <sample position="8">41666.666666666672</sample>
+              <sample position="9">43333.333333333336</sample>
+              <sample position="10">45000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/M">
@@ -711,16 +711,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">1.4</sample>
-              <sample position="2">1.42222222222</sample>
-              <sample position="3">1.44444444444</sample>
-              <sample position="4">1.46666666667</sample>
-              <sample position="5">1.48888888889</sample>
-              <sample position="6">1.51111111111</sample>
-              <sample position="7">1.53333333333</sample>
-              <sample position="8">1.55555555556</sample>
-              <sample position="9">1.57777777778</sample>
-              <sample position="10">1.6</sample>
+              <sample position="1">1.400000000000</sample>
+              <sample position="2">1.422222222222</sample>
+              <sample position="3">1.444444444444</sample>
+              <sample position="4">1.466666666667</sample>
+              <sample position="5">1.488888888889</sample>
+              <sample position="6">1.511111111111</sample>
+              <sample position="7">1.533333333333</sample>
+              <sample position="8">1.555555555556</sample>
+              <sample position="9">1.577777777778</sample>
+              <sample position="10">1.600000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/Lambda">
@@ -733,16 +733,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">40.0</sample>
-              <sample position="2">41.6666666667</sample>
-              <sample position="3">43.3333333333</sample>
-              <sample position="4">45.0</sample>
-              <sample position="5">46.6666666667</sample>
-              <sample position="6">48.3333333333</sample>
-              <sample position="7">50.0</sample>
-              <sample position="8">51.6666666667</sample>
-              <sample position="9">53.3333333333</sample>
-              <sample position="10">55.0</sample>
+              <sample position="1">40.000000000000</sample>
+              <sample position="2">41.666666666667</sample>
+              <sample position="3">43.333333333333</sample>
+              <sample position="4">45.000000000000</sample>
+              <sample position="5">46.666666666667</sample>
+              <sample position="6">48.333333333333</sample>
+              <sample position="7">50.000000000000</sample>
+              <sample position="8">51.666666666667</sample>
+              <sample position="9">53.333333333333</sample>
+              <sample position="10">55.000000000000</sample>
             </samples>
           </designVariable>
         </designVariables>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-J-CT.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-J-CT.xml
index 2e35af847ceea7c96084ff95f4cd371b4db92555..b8396bbe70d1c3da8fe1e01ab01a214a524fde4d 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-J-CT.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-DOE-J-CT.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-21T15:55:30.252183</timestamp>
+    <timestamp>2018-03-24T09:14:31.749000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-21T15:55:30.252183</timestamp>
+        <timestamp>2018-03-24T09:14:31.749000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -534,16 +534,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
-              <sample position="2">0.15</sample>
-              <sample position="3">0.2</sample>
-              <sample position="4">0.25</sample>
-              <sample position="5">0.3</sample>
-              <sample position="6">0.35</sample>
-              <sample position="7">0.4</sample>
-              <sample position="8">0.45</sample>
-              <sample position="9">0.5</sample>
-              <sample position="10">0.55</sample>
+              <sample position="1">0.100000000000</sample>
+              <sample position="2">0.150000000000</sample>
+              <sample position="3">0.200000000000</sample>
+              <sample position="4">0.250000000000</sample>
+              <sample position="5">0.300000000000</sample>
+              <sample position="6">0.350000000000</sample>
+              <sample position="7">0.400000000000</sample>
+              <sample position="8">0.450000000000</sample>
+              <sample position="9">0.500000000000</sample>
+              <sample position="10">0.550000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/other/Cf">
@@ -556,7 +556,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -565,7 +565,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/lambda">
@@ -578,16 +578,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
+              <sample position="1">0.100000000000</sample>
               <sample position="2">0.116666666667</sample>
               <sample position="3">0.133333333333</sample>
-              <sample position="4">0.15</sample>
+              <sample position="4">0.150000000000</sample>
               <sample position="5">0.166666666667</sample>
               <sample position="6">0.183333333333</sample>
-              <sample position="7">0.2</sample>
+              <sample position="7">0.200000000000</sample>
               <sample position="8">0.216666666667</sample>
               <sample position="9">0.233333333333</sample>
-              <sample position="10">0.25</sample>
+              <sample position="10">0.250000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/section">
@@ -600,7 +600,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -609,7 +609,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/AR">
@@ -622,16 +622,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">2.5</sample>
-              <sample position="2">2.83333333333</sample>
-              <sample position="3">3.16666666667</sample>
-              <sample position="4">3.5</sample>
-              <sample position="5">3.83333333333</sample>
-              <sample position="6">4.16666666667</sample>
-              <sample position="7">4.5</sample>
-              <sample position="8">4.83333333333</sample>
-              <sample position="9">5.16666666667</sample>
-              <sample position="10">5.5</sample>
+              <sample position="1">2.500000000000</sample>
+              <sample position="2">2.833333333333</sample>
+              <sample position="3">3.166666666667</sample>
+              <sample position="4">3.500000000000</sample>
+              <sample position="5">3.833333333333</sample>
+              <sample position="6">4.166666666667</sample>
+              <sample position="7">4.500000000000</sample>
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+              <sample position="10">5.500000000000</sample>
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           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/tc">
@@ -644,16 +644,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.01</sample>
-              <sample position="2">0.0144444444444</sample>
-              <sample position="3">0.0188888888889</sample>
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-              <sample position="5">0.0277777777778</sample>
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-              <sample position="7">0.0366666666667</sample>
-              <sample position="8">0.0411111111111</sample>
-              <sample position="9">0.0455555555556</sample>
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+              <sample position="1">0.010000000000</sample>
+              <sample position="2">0.014444444444</sample>
+              <sample position="3">0.018888888889</sample>
+              <sample position="4">0.023333333333</sample>
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+              <sample position="6">0.032222222222</sample>
+              <sample position="7">0.036666666667</sample>
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@@ -666,16 +666,16 @@
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@@ -688,16 +688,16 @@
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+              <sample position="1">500.000000000000</sample>
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@@ -710,16 +710,16 @@
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-              <sample position="7">40000.0</sample>
-              <sample position="8">41666.6666667</sample>
-              <sample position="9">43333.3333333</sample>
-              <sample position="10">45000.0</sample>
+              <sample position="1">30000.000000000000</sample>
+              <sample position="2">31666.666666666668</sample>
+              <sample position="3">33333.333333333336</sample>
+              <sample position="4">35000.000000000000</sample>
+              <sample position="5">36666.666666666664</sample>
+              <sample position="6">38333.333333333336</sample>
+              <sample position="7">40000.000000000000</sample>
+              <sample position="8">41666.666666666672</sample>
+              <sample position="9">43333.333333333336</sample>
+              <sample position="10">45000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/M">
@@ -732,16 +732,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">1.4</sample>
-              <sample position="2">1.42222222222</sample>
-              <sample position="3">1.44444444444</sample>
-              <sample position="4">1.46666666667</sample>
-              <sample position="5">1.48888888889</sample>
-              <sample position="6">1.51111111111</sample>
-              <sample position="7">1.53333333333</sample>
-              <sample position="8">1.55555555556</sample>
-              <sample position="9">1.57777777778</sample>
-              <sample position="10">1.6</sample>
+              <sample position="1">1.400000000000</sample>
+              <sample position="2">1.422222222222</sample>
+              <sample position="3">1.444444444444</sample>
+              <sample position="4">1.466666666667</sample>
+              <sample position="5">1.488888888889</sample>
+              <sample position="6">1.511111111111</sample>
+              <sample position="7">1.533333333333</sample>
+              <sample position="8">1.555555555556</sample>
+              <sample position="9">1.577777777778</sample>
+              <sample position="10">1.600000000000</sample>
             </samples>
           </designVariable>
         </designVariables>
@@ -1865,19 +1865,19 @@
             <doeMethod>Custom design table</doeMethod>
             <doeTable>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/lambda">
-                <tableElement experimentID="0">0.1</tableElement>
+                <tableElement experimentID="0">0.100000000000</tableElement>
                 <tableElement experimentID="1">0.116666666667</tableElement>
                 <tableElement experimentID="2">0.133333333333</tableElement>
-                <tableElement experimentID="3">0.15</tableElement>
+                <tableElement experimentID="3">0.150000000000</tableElement>
                 <tableElement experimentID="4">0.166666666667</tableElement>
                 <tableElement experimentID="5">0.183333333333</tableElement>
-                <tableElement experimentID="6">0.2</tableElement>
+                <tableElement experimentID="6">0.200000000000</tableElement>
                 <tableElement experimentID="7">0.216666666667</tableElement>
                 <tableElement experimentID="8">0.233333333333</tableElement>
-                <tableElement experimentID="9">0.25</tableElement>
+                <tableElement experimentID="9">0.250000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/section">
-                <tableElement experimentID="0">0.75</tableElement>
+                <tableElement experimentID="0">0.750000000000</tableElement>
                 <tableElement experimentID="1">0.777777777778</tableElement>
                 <tableElement experimentID="2">0.805555555556</tableElement>
                 <tableElement experimentID="3">0.833333333333</tableElement>
@@ -1886,10 +1886,10 @@
                 <tableElement experimentID="6">0.916666666667</tableElement>
                 <tableElement experimentID="7">0.944444444444</tableElement>
                 <tableElement experimentID="8">0.972222222222</tableElement>
-                <tableElement experimentID="9">1.0</tableElement>
+                <tableElement experimentID="9">1.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/other/Cf">
-                <tableElement experimentID="0">0.75</tableElement>
+                <tableElement experimentID="0">0.750000000000</tableElement>
                 <tableElement experimentID="1">0.777777777778</tableElement>
                 <tableElement experimentID="2">0.805555555556</tableElement>
                 <tableElement experimentID="3">0.833333333333</tableElement>
@@ -1898,91 +1898,91 @@
                 <tableElement experimentID="6">0.916666666667</tableElement>
                 <tableElement experimentID="7">0.944444444444</tableElement>
                 <tableElement experimentID="8">0.972222222222</tableElement>
-                <tableElement experimentID="9">1.0</tableElement>
+                <tableElement experimentID="9">1.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/other/T">
-                <tableElement experimentID="0">0.1</tableElement>
-                <tableElement experimentID="1">0.15</tableElement>
-                <tableElement experimentID="2">0.2</tableElement>
-                <tableElement experimentID="3">0.25</tableElement>
-                <tableElement experimentID="4">0.3</tableElement>
-                <tableElement experimentID="5">0.35</tableElement>
-                <tableElement experimentID="6">0.4</tableElement>
-                <tableElement experimentID="7">0.45</tableElement>
-                <tableElement experimentID="8">0.5</tableElement>
-                <tableElement experimentID="9">0.55</tableElement>
+                <tableElement experimentID="0">0.100000000000</tableElement>
+                <tableElement experimentID="1">0.150000000000</tableElement>
+                <tableElement experimentID="2">0.200000000000</tableElement>
+                <tableElement experimentID="3">0.250000000000</tableElement>
+                <tableElement experimentID="4">0.300000000000</tableElement>
+                <tableElement experimentID="5">0.350000000000</tableElement>
+                <tableElement experimentID="6">0.400000000000</tableElement>
+                <tableElement experimentID="7">0.450000000000</tableElement>
+                <tableElement experimentID="8">0.500000000000</tableElement>
+                <tableElement experimentID="9">0.550000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/AR">
-                <tableElement experimentID="0">2.5</tableElement>
-                <tableElement experimentID="1">2.83333333333</tableElement>
-                <tableElement experimentID="2">3.16666666667</tableElement>
-                <tableElement experimentID="3">3.5</tableElement>
-                <tableElement experimentID="4">3.83333333333</tableElement>
-                <tableElement experimentID="5">4.16666666667</tableElement>
-                <tableElement experimentID="6">4.5</tableElement>
-                <tableElement experimentID="7">4.83333333333</tableElement>
-                <tableElement experimentID="8">5.16666666667</tableElement>
-                <tableElement experimentID="9">5.5</tableElement>
+                <tableElement experimentID="0">2.500000000000</tableElement>
+                <tableElement experimentID="1">2.833333333333</tableElement>
+                <tableElement experimentID="2">3.166666666667</tableElement>
+                <tableElement experimentID="3">3.500000000000</tableElement>
+                <tableElement experimentID="4">3.833333333333</tableElement>
+                <tableElement experimentID="5">4.166666666667</tableElement>
+                <tableElement experimentID="6">4.500000000000</tableElement>
+                <tableElement experimentID="7">4.833333333333</tableElement>
+                <tableElement experimentID="8">5.166666666667</tableElement>
+                <tableElement experimentID="9">5.500000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/Lambda">
-                <tableElement experimentID="0">40.0</tableElement>
-                <tableElement experimentID="1">41.6666666667</tableElement>
-                <tableElement experimentID="2">43.3333333333</tableElement>
-                <tableElement experimentID="3">45.0</tableElement>
-                <tableElement experimentID="4">46.6666666667</tableElement>
-                <tableElement experimentID="5">48.3333333333</tableElement>
-                <tableElement experimentID="6">50.0</tableElement>
-                <tableElement experimentID="7">51.6666666667</tableElement>
-                <tableElement experimentID="8">53.3333333333</tableElement>
-                <tableElement experimentID="9">55.0</tableElement>
+                <tableElement experimentID="0">40.000000000000</tableElement>
+                <tableElement experimentID="1">41.666666666667</tableElement>
+                <tableElement experimentID="2">43.333333333333</tableElement>
+                <tableElement experimentID="3">45.000000000000</tableElement>
+                <tableElement experimentID="4">46.666666666667</tableElement>
+                <tableElement experimentID="5">48.333333333333</tableElement>
+                <tableElement experimentID="6">50.000000000000</tableElement>
+                <tableElement experimentID="7">51.666666666667</tableElement>
+                <tableElement experimentID="8">53.333333333333</tableElement>
+                <tableElement experimentID="9">55.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/Sref">
-                <tableElement experimentID="0">500.0</tableElement>
-                <tableElement experimentID="1">555.555555556</tableElement>
-                <tableElement experimentID="2">611.111111111</tableElement>
-                <tableElement experimentID="3">666.666666667</tableElement>
-                <tableElement experimentID="4">722.222222222</tableElement>
-                <tableElement experimentID="5">777.777777778</tableElement>
-                <tableElement experimentID="6">833.333333333</tableElement>
-                <tableElement experimentID="7">888.888888889</tableElement>
-                <tableElement experimentID="8">944.444444444</tableElement>
-                <tableElement experimentID="9">1000.0</tableElement>
+                <tableElement experimentID="0">500.000000000000</tableElement>
+                <tableElement experimentID="1">555.555555555556</tableElement>
+                <tableElement experimentID="2">611.111111111111</tableElement>
+                <tableElement experimentID="3">666.666666666667</tableElement>
+                <tableElement experimentID="4">722.222222222222</tableElement>
+                <tableElement experimentID="5">777.777777777778</tableElement>
+                <tableElement experimentID="6">833.333333333333</tableElement>
+                <tableElement experimentID="7">888.888888888889</tableElement>
+                <tableElement experimentID="8">944.444444444444</tableElement>
+                <tableElement experimentID="9">1000.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/tc">
-                <tableElement experimentID="0">0.01</tableElement>
-                <tableElement experimentID="1">0.0144444444444</tableElement>
-                <tableElement experimentID="2">0.0188888888889</tableElement>
-                <tableElement experimentID="3">0.0233333333333</tableElement>
-                <tableElement experimentID="4">0.0277777777778</tableElement>
-                <tableElement experimentID="5">0.0322222222222</tableElement>
-                <tableElement experimentID="6">0.0366666666667</tableElement>
-                <tableElement experimentID="7">0.0411111111111</tableElement>
-                <tableElement experimentID="8">0.0455555555556</tableElement>
-                <tableElement experimentID="9">0.05</tableElement>
+                <tableElement experimentID="0">0.010000000000</tableElement>
+                <tableElement experimentID="1">0.014444444444</tableElement>
+                <tableElement experimentID="2">0.018888888889</tableElement>
+                <tableElement experimentID="3">0.023333333333</tableElement>
+                <tableElement experimentID="4">0.027777777778</tableElement>
+                <tableElement experimentID="5">0.032222222222</tableElement>
+                <tableElement experimentID="6">0.036666666667</tableElement>
+                <tableElement experimentID="7">0.041111111111</tableElement>
+                <tableElement experimentID="8">0.045555555556</tableElement>
+                <tableElement experimentID="9">0.050000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/reference/h">
-                <tableElement experimentID="0">30000.0</tableElement>
-                <tableElement experimentID="1">31666.6666667</tableElement>
-                <tableElement experimentID="2">33333.3333333</tableElement>
-                <tableElement experimentID="3">35000.0</tableElement>
-                <tableElement experimentID="4">36666.6666667</tableElement>
-                <tableElement experimentID="5">38333.3333333</tableElement>
-                <tableElement experimentID="6">40000.0</tableElement>
-                <tableElement experimentID="7">41666.6666667</tableElement>
-                <tableElement experimentID="8">43333.3333333</tableElement>
-                <tableElement experimentID="9">45000.0</tableElement>
+                <tableElement experimentID="0">30000.000000000000</tableElement>
+                <tableElement experimentID="1">31666.666666666668</tableElement>
+                <tableElement experimentID="2">33333.333333333336</tableElement>
+                <tableElement experimentID="3">35000.000000000000</tableElement>
+                <tableElement experimentID="4">36666.666666666664</tableElement>
+                <tableElement experimentID="5">38333.333333333336</tableElement>
+                <tableElement experimentID="6">40000.000000000000</tableElement>
+                <tableElement experimentID="7">41666.666666666672</tableElement>
+                <tableElement experimentID="8">43333.333333333336</tableElement>
+                <tableElement experimentID="9">45000.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/reference/M">
-                <tableElement experimentID="0">1.4</tableElement>
-                <tableElement experimentID="1">1.42222222222</tableElement>
-                <tableElement experimentID="2">1.44444444444</tableElement>
-                <tableElement experimentID="3">1.46666666667</tableElement>
-                <tableElement experimentID="4">1.48888888889</tableElement>
-                <tableElement experimentID="5">1.51111111111</tableElement>
-                <tableElement experimentID="6">1.53333333333</tableElement>
-                <tableElement experimentID="7">1.55555555556</tableElement>
-                <tableElement experimentID="8">1.57777777778</tableElement>
-                <tableElement experimentID="9">1.6</tableElement>
+                <tableElement experimentID="0">1.400000000000</tableElement>
+                <tableElement experimentID="1">1.422222222222</tableElement>
+                <tableElement experimentID="2">1.444444444444</tableElement>
+                <tableElement experimentID="3">1.466666666667</tableElement>
+                <tableElement experimentID="4">1.488888888889</tableElement>
+                <tableElement experimentID="5">1.511111111111</tableElement>
+                <tableElement experimentID="6">1.533333333333</tableElement>
+                <tableElement experimentID="7">1.555555555556</tableElement>
+                <tableElement experimentID="8">1.577777777778</tableElement>
+                <tableElement experimentID="9">1.600000000000</tableElement>
               </tableRow>
             </doeTable>
           </settings>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-GS.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-GS.xml
index a57206d74af46798c3b2163300ac14883f75b865..b8fd805eca7c3061c7a98b63348252731de67da2 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-GS.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-GS.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-21T15:55:30.252183</timestamp>
+    <timestamp>2018-03-24T09:14:31.749000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-21T15:55:30.252183</timestamp>
+        <timestamp>2018-03-24T09:14:31.749000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-J.xml b/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-J.xml
index 2d3c77243191d4def13dfbf72f88d38350a5a576..13c7f72b7c3923885982ac2261d697a8d9b428d8 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-J.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_converged-MDA-J.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-21T15:55:30.252183</timestamp>
+    <timestamp>2018-03-24T09:14:31.749000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-21T15:55:30.252183</timestamp>
+        <timestamp>2018-03-24T09:14:31.749000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-GS-CT.xml b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-GS-CT.xml
index 3fbd54ae7b224b45f8ce6337aaa8daa7b20fe0bf..30199d6144a0b9b8ffef9dd48ea0a5aa2c467d13 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-GS-CT.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-GS-CT.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-21T15:55:30.252183</timestamp>
+    <timestamp>2018-03-24T09:14:31.749000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-21T15:55:30.252183</timestamp>
+        <timestamp>2018-03-24T09:14:31.749000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -422,9 +422,6 @@
     <parameter uID="/data_schema/mdo_data/objectives/R">
       <label>R</label>
     </parameter>
-    <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma5">
-      <label>sigma5</label>
-    </parameter>
     <parameter uID="/data_schema/aircraft/weight/WO">
       <label>WO</label>
     </parameter>
@@ -458,6 +455,9 @@
     <parameter uID="/data_schema/reference/Temp">
       <label>Temp</label>
     </parameter>
+    <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma5">
+      <label>sigma5</label>
+    </parameter>
     <parameter uID="/data_schema/aircraft/other/fin">
       <label>fin</label>
     </parameter>
@@ -525,16 +525,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
+              <sample position="1">0.100000000000</sample>
               <sample position="2">0.116666666667</sample>
               <sample position="3">0.133333333333</sample>
-              <sample position="4">0.15</sample>
+              <sample position="4">0.150000000000</sample>
               <sample position="5">0.166666666667</sample>
               <sample position="6">0.183333333333</sample>
-              <sample position="7">0.2</sample>
+              <sample position="7">0.200000000000</sample>
               <sample position="8">0.216666666667</sample>
               <sample position="9">0.233333333333</sample>
-              <sample position="10">0.25</sample>
+              <sample position="10">0.250000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/section">
@@ -547,7 +547,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -556,7 +556,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/other/Cf">
@@ -569,7 +569,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -578,7 +578,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/other/T">
@@ -591,16 +591,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
-              <sample position="2">0.15</sample>
-              <sample position="3">0.2</sample>
-              <sample position="4">0.25</sample>
-              <sample position="5">0.3</sample>
-              <sample position="6">0.35</sample>
-              <sample position="7">0.4</sample>
-              <sample position="8">0.45</sample>
-              <sample position="9">0.5</sample>
-              <sample position="10">0.55</sample>
+              <sample position="1">0.100000000000</sample>
+              <sample position="2">0.150000000000</sample>
+              <sample position="3">0.200000000000</sample>
+              <sample position="4">0.250000000000</sample>
+              <sample position="5">0.300000000000</sample>
+              <sample position="6">0.350000000000</sample>
+              <sample position="7">0.400000000000</sample>
+              <sample position="8">0.450000000000</sample>
+              <sample position="9">0.500000000000</sample>
+              <sample position="10">0.550000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/AR">
@@ -613,16 +613,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">2.5</sample>
-              <sample position="2">2.83333333333</sample>
-              <sample position="3">3.16666666667</sample>
-              <sample position="4">3.5</sample>
-              <sample position="5">3.83333333333</sample>
-              <sample position="6">4.16666666667</sample>
-              <sample position="7">4.5</sample>
-              <sample position="8">4.83333333333</sample>
-              <sample position="9">5.16666666667</sample>
-              <sample position="10">5.5</sample>
+              <sample position="1">2.500000000000</sample>
+              <sample position="2">2.833333333333</sample>
+              <sample position="3">3.166666666667</sample>
+              <sample position="4">3.500000000000</sample>
+              <sample position="5">3.833333333333</sample>
+              <sample position="6">4.166666666667</sample>
+              <sample position="7">4.500000000000</sample>
+              <sample position="8">4.833333333333</sample>
+              <sample position="9">5.166666666667</sample>
+              <sample position="10">5.500000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/Sref">
@@ -635,16 +635,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">500.0</sample>
-              <sample position="2">555.555555556</sample>
-              <sample position="3">611.111111111</sample>
-              <sample position="4">666.666666667</sample>
-              <sample position="5">722.222222222</sample>
-              <sample position="6">777.777777778</sample>
-              <sample position="7">833.333333333</sample>
-              <sample position="8">888.888888889</sample>
-              <sample position="9">944.444444444</sample>
-              <sample position="10">1000.0</sample>
+              <sample position="1">500.000000000000</sample>
+              <sample position="2">555.555555555556</sample>
+              <sample position="3">611.111111111111</sample>
+              <sample position="4">666.666666666667</sample>
+              <sample position="5">722.222222222222</sample>
+              <sample position="6">777.777777777778</sample>
+              <sample position="7">833.333333333333</sample>
+              <sample position="8">888.888888888889</sample>
+              <sample position="9">944.444444444444</sample>
+              <sample position="10">1000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/tc">
@@ -657,16 +657,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.01</sample>
-              <sample position="2">0.0144444444444</sample>
-              <sample position="3">0.0188888888889</sample>
-              <sample position="4">0.0233333333333</sample>
-              <sample position="5">0.0277777777778</sample>
-              <sample position="6">0.0322222222222</sample>
-              <sample position="7">0.0366666666667</sample>
-              <sample position="8">0.0411111111111</sample>
-              <sample position="9">0.0455555555556</sample>
-              <sample position="10">0.05</sample>
+              <sample position="1">0.010000000000</sample>
+              <sample position="2">0.014444444444</sample>
+              <sample position="3">0.018888888889</sample>
+              <sample position="4">0.023333333333</sample>
+              <sample position="5">0.027777777778</sample>
+              <sample position="6">0.032222222222</sample>
+              <sample position="7">0.036666666667</sample>
+              <sample position="8">0.041111111111</sample>
+              <sample position="9">0.045555555556</sample>
+              <sample position="10">0.050000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/Lambda">
@@ -679,16 +679,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">40.0</sample>
-              <sample position="2">41.6666666667</sample>
-              <sample position="3">43.3333333333</sample>
-              <sample position="4">45.0</sample>
-              <sample position="5">46.6666666667</sample>
-              <sample position="6">48.3333333333</sample>
-              <sample position="7">50.0</sample>
-              <sample position="8">51.6666666667</sample>
-              <sample position="9">53.3333333333</sample>
-              <sample position="10">55.0</sample>
+              <sample position="1">40.000000000000</sample>
+              <sample position="2">41.666666666667</sample>
+              <sample position="3">43.333333333333</sample>
+              <sample position="4">45.000000000000</sample>
+              <sample position="5">46.666666666667</sample>
+              <sample position="6">48.333333333333</sample>
+              <sample position="7">50.000000000000</sample>
+              <sample position="8">51.666666666667</sample>
+              <sample position="9">53.333333333333</sample>
+              <sample position="10">55.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/h">
@@ -701,16 +701,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">30000.0</sample>
-              <sample position="2">31666.6666667</sample>
-              <sample position="3">33333.3333333</sample>
-              <sample position="4">35000.0</sample>
-              <sample position="5">36666.6666667</sample>
-              <sample position="6">38333.3333333</sample>
-              <sample position="7">40000.0</sample>
-              <sample position="8">41666.6666667</sample>
-              <sample position="9">43333.3333333</sample>
-              <sample position="10">45000.0</sample>
+              <sample position="1">30000.000000000000</sample>
+              <sample position="2">31666.666666666668</sample>
+              <sample position="3">33333.333333333336</sample>
+              <sample position="4">35000.000000000000</sample>
+              <sample position="5">36666.666666666664</sample>
+              <sample position="6">38333.333333333336</sample>
+              <sample position="7">40000.000000000000</sample>
+              <sample position="8">41666.666666666672</sample>
+              <sample position="9">43333.333333333336</sample>
+              <sample position="10">45000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/M">
@@ -723,16 +723,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">1.4</sample>
-              <sample position="2">1.42222222222</sample>
-              <sample position="3">1.44444444444</sample>
-              <sample position="4">1.46666666667</sample>
-              <sample position="5">1.48888888889</sample>
-              <sample position="6">1.51111111111</sample>
-              <sample position="7">1.53333333333</sample>
-              <sample position="8">1.55555555556</sample>
-              <sample position="9">1.57777777778</sample>
-              <sample position="10">1.6</sample>
+              <sample position="1">1.400000000000</sample>
+              <sample position="2">1.422222222222</sample>
+              <sample position="3">1.444444444444</sample>
+              <sample position="4">1.466666666667</sample>
+              <sample position="5">1.488888888889</sample>
+              <sample position="6">1.511111111111</sample>
+              <sample position="7">1.533333333333</sample>
+              <sample position="8">1.555555555556</sample>
+              <sample position="9">1.577777777778</sample>
+              <sample position="10">1.600000000000</sample>
             </samples>
           </designVariable>
         </designVariables>
@@ -761,9 +761,6 @@
           <stateVariable uID="__statVar__/data_schema/mdo_data/objectives/R">
             <parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
           </stateVariable>
-          <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma5">
-            <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
-          </stateVariable>
           <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
             <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
           </stateVariable>
@@ -773,6 +770,9 @@
           <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/DT">
             <parameterUID>/data_schema/mdo_data/constraints/propulsion/DT</parameterUID>
           </stateVariable>
+          <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma5">
+            <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
+          </stateVariable>
         </stateVariables>
       </parameters>
       <executableBlocks>
@@ -1085,6 +1085,10 @@
           <fromParameterUID>/data_schema/aircraft/other/R</fromParameterUID>
           <toExecutableBlockUID>F[R]</toExecutableBlockUID>
         </edge>
+        <edge>
+          <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR</fromParameterUID>
+          <toExecutableBlockUID>DOE</toExecutableBlockUID>
+        </edge>
         <edge>
           <fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/other/L</fromParameterUID>
           <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
@@ -1129,10 +1133,6 @@
           <fromParameterUID>/data_schema/aircraft/geometry/tc</fromParameterUID>
           <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
         </edge>
-        <edge>
-          <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</fromParameterUID>
-          <toExecutableBlockUID>DOE</toExecutableBlockUID>
-        </edge>
         <edge>
           <fromParameterUID>/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/mdo_data/constraints/Theta</fromParameterUID>
           <toExecutableBlockUID>Coordinator</toExecutableBlockUID>
@@ -1358,7 +1358,7 @@
           <toExecutableBlockUID>DOE</toExecutableBlockUID>
         </edge>
         <edge>
-          <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR</fromParameterUID>
+          <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</fromParameterUID>
           <toExecutableBlockUID>DOE</toExecutableBlockUID>
         </edge>
         <edge>
@@ -1588,6 +1588,10 @@
           <relatedParameterUID>/data_schema/reference/h</relatedParameterUID>
           <label>DOE_h_{inp}</label>
         </doeInputSampleList>
+        <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR">
+          <relatedParameterUID>/data_schema/aircraft/geometry/AR</relatedParameterUID>
+          <label>DOE_AR_{inp}</label>
+        </doeInputSampleList>
         <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/reference/M">
           <relatedParameterUID>/data_schema/reference/M</relatedParameterUID>
           <label>DOE_M_{inp}</label>
@@ -1604,10 +1608,6 @@
           <relatedParameterUID>/data_schema/aircraft/other/T</relatedParameterUID>
           <label>DOE_T_{inp}</label>
         </doeInputSampleList>
-        <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR">
-          <relatedParameterUID>/data_schema/aircraft/geometry/AR</relatedParameterUID>
-          <label>DOE_AR_{inp}</label>
-        </doeInputSampleList>
       </doeInputSampleLists>
       <doeOutputSampleLists>
         <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE">
@@ -1673,19 +1673,19 @@
             <doeMethod>Custom design table</doeMethod>
             <doeTable>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/lambda">
-                <tableElement experimentID="0">0.1</tableElement>
+                <tableElement experimentID="0">0.100000000000</tableElement>
                 <tableElement experimentID="1">0.116666666667</tableElement>
                 <tableElement experimentID="2">0.133333333333</tableElement>
-                <tableElement experimentID="3">0.15</tableElement>
+                <tableElement experimentID="3">0.150000000000</tableElement>
                 <tableElement experimentID="4">0.166666666667</tableElement>
                 <tableElement experimentID="5">0.183333333333</tableElement>
-                <tableElement experimentID="6">0.2</tableElement>
+                <tableElement experimentID="6">0.200000000000</tableElement>
                 <tableElement experimentID="7">0.216666666667</tableElement>
                 <tableElement experimentID="8">0.233333333333</tableElement>
-                <tableElement experimentID="9">0.25</tableElement>
+                <tableElement experimentID="9">0.250000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/section">
-                <tableElement experimentID="0">0.75</tableElement>
+                <tableElement experimentID="0">0.750000000000</tableElement>
                 <tableElement experimentID="1">0.777777777778</tableElement>
                 <tableElement experimentID="2">0.805555555556</tableElement>
                 <tableElement experimentID="3">0.833333333333</tableElement>
@@ -1694,10 +1694,10 @@
                 <tableElement experimentID="6">0.916666666667</tableElement>
                 <tableElement experimentID="7">0.944444444444</tableElement>
                 <tableElement experimentID="8">0.972222222222</tableElement>
-                <tableElement experimentID="9">1.0</tableElement>
+                <tableElement experimentID="9">1.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/other/Cf">
-                <tableElement experimentID="0">0.75</tableElement>
+                <tableElement experimentID="0">0.750000000000</tableElement>
                 <tableElement experimentID="1">0.777777777778</tableElement>
                 <tableElement experimentID="2">0.805555555556</tableElement>
                 <tableElement experimentID="3">0.833333333333</tableElement>
@@ -1706,91 +1706,91 @@
                 <tableElement experimentID="6">0.916666666667</tableElement>
                 <tableElement experimentID="7">0.944444444444</tableElement>
                 <tableElement experimentID="8">0.972222222222</tableElement>
-                <tableElement experimentID="9">1.0</tableElement>
+                <tableElement experimentID="9">1.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/other/T">
-                <tableElement experimentID="0">0.1</tableElement>
-                <tableElement experimentID="1">0.15</tableElement>
-                <tableElement experimentID="2">0.2</tableElement>
-                <tableElement experimentID="3">0.25</tableElement>
-                <tableElement experimentID="4">0.3</tableElement>
-                <tableElement experimentID="5">0.35</tableElement>
-                <tableElement experimentID="6">0.4</tableElement>
-                <tableElement experimentID="7">0.45</tableElement>
-                <tableElement experimentID="8">0.5</tableElement>
-                <tableElement experimentID="9">0.55</tableElement>
+                <tableElement experimentID="0">0.100000000000</tableElement>
+                <tableElement experimentID="1">0.150000000000</tableElement>
+                <tableElement experimentID="2">0.200000000000</tableElement>
+                <tableElement experimentID="3">0.250000000000</tableElement>
+                <tableElement experimentID="4">0.300000000000</tableElement>
+                <tableElement experimentID="5">0.350000000000</tableElement>
+                <tableElement experimentID="6">0.400000000000</tableElement>
+                <tableElement experimentID="7">0.450000000000</tableElement>
+                <tableElement experimentID="8">0.500000000000</tableElement>
+                <tableElement experimentID="9">0.550000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/AR">
-                <tableElement experimentID="0">2.5</tableElement>
-                <tableElement experimentID="1">2.83333333333</tableElement>
-                <tableElement experimentID="2">3.16666666667</tableElement>
-                <tableElement experimentID="3">3.5</tableElement>
-                <tableElement experimentID="4">3.83333333333</tableElement>
-                <tableElement experimentID="5">4.16666666667</tableElement>
-                <tableElement experimentID="6">4.5</tableElement>
-                <tableElement experimentID="7">4.83333333333</tableElement>
-                <tableElement experimentID="8">5.16666666667</tableElement>
-                <tableElement experimentID="9">5.5</tableElement>
+                <tableElement experimentID="0">2.500000000000</tableElement>
+                <tableElement experimentID="1">2.833333333333</tableElement>
+                <tableElement experimentID="2">3.166666666667</tableElement>
+                <tableElement experimentID="3">3.500000000000</tableElement>
+                <tableElement experimentID="4">3.833333333333</tableElement>
+                <tableElement experimentID="5">4.166666666667</tableElement>
+                <tableElement experimentID="6">4.500000000000</tableElement>
+                <tableElement experimentID="7">4.833333333333</tableElement>
+                <tableElement experimentID="8">5.166666666667</tableElement>
+                <tableElement experimentID="9">5.500000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/Lambda">
-                <tableElement experimentID="0">40.0</tableElement>
-                <tableElement experimentID="1">41.6666666667</tableElement>
-                <tableElement experimentID="2">43.3333333333</tableElement>
-                <tableElement experimentID="3">45.0</tableElement>
-                <tableElement experimentID="4">46.6666666667</tableElement>
-                <tableElement experimentID="5">48.3333333333</tableElement>
-                <tableElement experimentID="6">50.0</tableElement>
-                <tableElement experimentID="7">51.6666666667</tableElement>
-                <tableElement experimentID="8">53.3333333333</tableElement>
-                <tableElement experimentID="9">55.0</tableElement>
+                <tableElement experimentID="0">40.000000000000</tableElement>
+                <tableElement experimentID="1">41.666666666667</tableElement>
+                <tableElement experimentID="2">43.333333333333</tableElement>
+                <tableElement experimentID="3">45.000000000000</tableElement>
+                <tableElement experimentID="4">46.666666666667</tableElement>
+                <tableElement experimentID="5">48.333333333333</tableElement>
+                <tableElement experimentID="6">50.000000000000</tableElement>
+                <tableElement experimentID="7">51.666666666667</tableElement>
+                <tableElement experimentID="8">53.333333333333</tableElement>
+                <tableElement experimentID="9">55.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/Sref">
-                <tableElement experimentID="0">500.0</tableElement>
-                <tableElement experimentID="1">555.555555556</tableElement>
-                <tableElement experimentID="2">611.111111111</tableElement>
-                <tableElement experimentID="3">666.666666667</tableElement>
-                <tableElement experimentID="4">722.222222222</tableElement>
-                <tableElement experimentID="5">777.777777778</tableElement>
-                <tableElement experimentID="6">833.333333333</tableElement>
-                <tableElement experimentID="7">888.888888889</tableElement>
-                <tableElement experimentID="8">944.444444444</tableElement>
-                <tableElement experimentID="9">1000.0</tableElement>
+                <tableElement experimentID="0">500.000000000000</tableElement>
+                <tableElement experimentID="1">555.555555555556</tableElement>
+                <tableElement experimentID="2">611.111111111111</tableElement>
+                <tableElement experimentID="3">666.666666666667</tableElement>
+                <tableElement experimentID="4">722.222222222222</tableElement>
+                <tableElement experimentID="5">777.777777777778</tableElement>
+                <tableElement experimentID="6">833.333333333333</tableElement>
+                <tableElement experimentID="7">888.888888888889</tableElement>
+                <tableElement experimentID="8">944.444444444444</tableElement>
+                <tableElement experimentID="9">1000.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/tc">
-                <tableElement experimentID="0">0.01</tableElement>
-                <tableElement experimentID="1">0.0144444444444</tableElement>
-                <tableElement experimentID="2">0.0188888888889</tableElement>
-                <tableElement experimentID="3">0.0233333333333</tableElement>
-                <tableElement experimentID="4">0.0277777777778</tableElement>
-                <tableElement experimentID="5">0.0322222222222</tableElement>
-                <tableElement experimentID="6">0.0366666666667</tableElement>
-                <tableElement experimentID="7">0.0411111111111</tableElement>
-                <tableElement experimentID="8">0.0455555555556</tableElement>
-                <tableElement experimentID="9">0.05</tableElement>
+                <tableElement experimentID="0">0.010000000000</tableElement>
+                <tableElement experimentID="1">0.014444444444</tableElement>
+                <tableElement experimentID="2">0.018888888889</tableElement>
+                <tableElement experimentID="3">0.023333333333</tableElement>
+                <tableElement experimentID="4">0.027777777778</tableElement>
+                <tableElement experimentID="5">0.032222222222</tableElement>
+                <tableElement experimentID="6">0.036666666667</tableElement>
+                <tableElement experimentID="7">0.041111111111</tableElement>
+                <tableElement experimentID="8">0.045555555556</tableElement>
+                <tableElement experimentID="9">0.050000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/reference/h">
-                <tableElement experimentID="0">30000.0</tableElement>
-                <tableElement experimentID="1">31666.6666667</tableElement>
-                <tableElement experimentID="2">33333.3333333</tableElement>
-                <tableElement experimentID="3">35000.0</tableElement>
-                <tableElement experimentID="4">36666.6666667</tableElement>
-                <tableElement experimentID="5">38333.3333333</tableElement>
-                <tableElement experimentID="6">40000.0</tableElement>
-                <tableElement experimentID="7">41666.6666667</tableElement>
-                <tableElement experimentID="8">43333.3333333</tableElement>
-                <tableElement experimentID="9">45000.0</tableElement>
+                <tableElement experimentID="0">30000.000000000000</tableElement>
+                <tableElement experimentID="1">31666.666666666668</tableElement>
+                <tableElement experimentID="2">33333.333333333336</tableElement>
+                <tableElement experimentID="3">35000.000000000000</tableElement>
+                <tableElement experimentID="4">36666.666666666664</tableElement>
+                <tableElement experimentID="5">38333.333333333336</tableElement>
+                <tableElement experimentID="6">40000.000000000000</tableElement>
+                <tableElement experimentID="7">41666.666666666672</tableElement>
+                <tableElement experimentID="8">43333.333333333336</tableElement>
+                <tableElement experimentID="9">45000.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/reference/M">
-                <tableElement experimentID="0">1.4</tableElement>
-                <tableElement experimentID="1">1.42222222222</tableElement>
-                <tableElement experimentID="2">1.44444444444</tableElement>
-                <tableElement experimentID="3">1.46666666667</tableElement>
-                <tableElement experimentID="4">1.48888888889</tableElement>
-                <tableElement experimentID="5">1.51111111111</tableElement>
-                <tableElement experimentID="6">1.53333333333</tableElement>
-                <tableElement experimentID="7">1.55555555556</tableElement>
-                <tableElement experimentID="8">1.57777777778</tableElement>
-                <tableElement experimentID="9">1.6</tableElement>
+                <tableElement experimentID="0">1.400000000000</tableElement>
+                <tableElement experimentID="1">1.422222222222</tableElement>
+                <tableElement experimentID="2">1.444444444444</tableElement>
+                <tableElement experimentID="3">1.466666666667</tableElement>
+                <tableElement experimentID="4">1.488888888889</tableElement>
+                <tableElement experimentID="5">1.511111111111</tableElement>
+                <tableElement experimentID="6">1.533333333333</tableElement>
+                <tableElement experimentID="7">1.555555555556</tableElement>
+                <tableElement experimentID="8">1.577777777778</tableElement>
+                <tableElement experimentID="9">1.600000000000</tableElement>
               </tableRow>
             </doeTable>
           </settings>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-J-CT.xml b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-J-CT.xml
index b0bb7f4b0d5a562fb1742d292d00efaa4b0ca3ef..1b2ae12a1f62561a54d887907ec687dec152b704 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-J-CT.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-DOE-J-CT.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-21T15:55:30.252183</timestamp>
+    <timestamp>2018-03-24T09:14:31.749000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-21T15:55:30.252183</timestamp>
+        <timestamp>2018-03-24T09:14:31.749000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
@@ -428,9 +428,6 @@
     <parameter uID="/data_schema/mdo_data/objectives/R">
       <label>R</label>
     </parameter>
-    <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma5">
-      <label>sigma5</label>
-    </parameter>
     <parameter uID="/data_schema/aircraft/weight/WO">
       <label>WO</label>
     </parameter>
@@ -455,6 +452,9 @@
     <parameter uID="/data_schema/aircraft/other/Cf">
       <label>Cf</label>
     </parameter>
+    <parameter uID="/data_schema/mdo_data/constraints/sigmas/sigma5">
+      <label>sigma5</label>
+    </parameter>
     <parameter uID="/data_schema/reference/Temp">
       <label>Temp</label>
     </parameter>
@@ -519,16 +519,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
+              <sample position="1">0.100000000000</sample>
               <sample position="2">0.116666666667</sample>
               <sample position="3">0.133333333333</sample>
-              <sample position="4">0.15</sample>
+              <sample position="4">0.150000000000</sample>
               <sample position="5">0.166666666667</sample>
               <sample position="6">0.183333333333</sample>
-              <sample position="7">0.2</sample>
+              <sample position="7">0.200000000000</sample>
               <sample position="8">0.216666666667</sample>
               <sample position="9">0.233333333333</sample>
-              <sample position="10">0.25</sample>
+              <sample position="10">0.250000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/section">
@@ -541,7 +541,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -550,7 +550,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/other/Cf">
@@ -563,7 +563,7 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.75</sample>
+              <sample position="1">0.750000000000</sample>
               <sample position="2">0.777777777778</sample>
               <sample position="3">0.805555555556</sample>
               <sample position="4">0.833333333333</sample>
@@ -572,7 +572,7 @@
               <sample position="7">0.916666666667</sample>
               <sample position="8">0.944444444444</sample>
               <sample position="9">0.972222222222</sample>
-              <sample position="10">1.0</sample>
+              <sample position="10">1.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/other/T">
@@ -585,16 +585,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.1</sample>
-              <sample position="2">0.15</sample>
-              <sample position="3">0.2</sample>
-              <sample position="4">0.25</sample>
-              <sample position="5">0.3</sample>
-              <sample position="6">0.35</sample>
-              <sample position="7">0.4</sample>
-              <sample position="8">0.45</sample>
-              <sample position="9">0.5</sample>
-              <sample position="10">0.55</sample>
+              <sample position="1">0.100000000000</sample>
+              <sample position="2">0.150000000000</sample>
+              <sample position="3">0.200000000000</sample>
+              <sample position="4">0.250000000000</sample>
+              <sample position="5">0.300000000000</sample>
+              <sample position="6">0.350000000000</sample>
+              <sample position="7">0.400000000000</sample>
+              <sample position="8">0.450000000000</sample>
+              <sample position="9">0.500000000000</sample>
+              <sample position="10">0.550000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/AR">
@@ -607,16 +607,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">2.5</sample>
-              <sample position="2">2.83333333333</sample>
-              <sample position="3">3.16666666667</sample>
-              <sample position="4">3.5</sample>
-              <sample position="5">3.83333333333</sample>
-              <sample position="6">4.16666666667</sample>
-              <sample position="7">4.5</sample>
-              <sample position="8">4.83333333333</sample>
-              <sample position="9">5.16666666667</sample>
-              <sample position="10">5.5</sample>
+              <sample position="1">2.500000000000</sample>
+              <sample position="2">2.833333333333</sample>
+              <sample position="3">3.166666666667</sample>
+              <sample position="4">3.500000000000</sample>
+              <sample position="5">3.833333333333</sample>
+              <sample position="6">4.166666666667</sample>
+              <sample position="7">4.500000000000</sample>
+              <sample position="8">4.833333333333</sample>
+              <sample position="9">5.166666666667</sample>
+              <sample position="10">5.500000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/Sref">
@@ -629,16 +629,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">500.0</sample>
-              <sample position="2">555.555555556</sample>
-              <sample position="3">611.111111111</sample>
-              <sample position="4">666.666666667</sample>
-              <sample position="5">722.222222222</sample>
-              <sample position="6">777.777777778</sample>
-              <sample position="7">833.333333333</sample>
-              <sample position="8">888.888888889</sample>
-              <sample position="9">944.444444444</sample>
-              <sample position="10">1000.0</sample>
+              <sample position="1">500.000000000000</sample>
+              <sample position="2">555.555555555556</sample>
+              <sample position="3">611.111111111111</sample>
+              <sample position="4">666.666666666667</sample>
+              <sample position="5">722.222222222222</sample>
+              <sample position="6">777.777777777778</sample>
+              <sample position="7">833.333333333333</sample>
+              <sample position="8">888.888888888889</sample>
+              <sample position="9">944.444444444444</sample>
+              <sample position="10">1000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/tc">
@@ -651,16 +651,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">0.01</sample>
-              <sample position="2">0.0144444444444</sample>
-              <sample position="3">0.0188888888889</sample>
-              <sample position="4">0.0233333333333</sample>
-              <sample position="5">0.0277777777778</sample>
-              <sample position="6">0.0322222222222</sample>
-              <sample position="7">0.0366666666667</sample>
-              <sample position="8">0.0411111111111</sample>
-              <sample position="9">0.0455555555556</sample>
-              <sample position="10">0.05</sample>
+              <sample position="1">0.010000000000</sample>
+              <sample position="2">0.014444444444</sample>
+              <sample position="3">0.018888888889</sample>
+              <sample position="4">0.023333333333</sample>
+              <sample position="5">0.027777777778</sample>
+              <sample position="6">0.032222222222</sample>
+              <sample position="7">0.036666666667</sample>
+              <sample position="8">0.041111111111</sample>
+              <sample position="9">0.045555555556</sample>
+              <sample position="10">0.050000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/h">
@@ -673,16 +673,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">30000.0</sample>
-              <sample position="2">31666.6666667</sample>
-              <sample position="3">33333.3333333</sample>
-              <sample position="4">35000.0</sample>
-              <sample position="5">36666.6666667</sample>
-              <sample position="6">38333.3333333</sample>
-              <sample position="7">40000.0</sample>
-              <sample position="8">41666.6666667</sample>
-              <sample position="9">43333.3333333</sample>
-              <sample position="10">45000.0</sample>
+              <sample position="1">30000.000000000000</sample>
+              <sample position="2">31666.666666666668</sample>
+              <sample position="3">33333.333333333336</sample>
+              <sample position="4">35000.000000000000</sample>
+              <sample position="5">36666.666666666664</sample>
+              <sample position="6">38333.333333333336</sample>
+              <sample position="7">40000.000000000000</sample>
+              <sample position="8">41666.666666666672</sample>
+              <sample position="9">43333.333333333336</sample>
+              <sample position="10">45000.000000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/reference/M">
@@ -695,16 +695,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">1.4</sample>
-              <sample position="2">1.42222222222</sample>
-              <sample position="3">1.44444444444</sample>
-              <sample position="4">1.46666666667</sample>
-              <sample position="5">1.48888888889</sample>
-              <sample position="6">1.51111111111</sample>
-              <sample position="7">1.53333333333</sample>
-              <sample position="8">1.55555555556</sample>
-              <sample position="9">1.57777777778</sample>
-              <sample position="10">1.6</sample>
+              <sample position="1">1.400000000000</sample>
+              <sample position="2">1.422222222222</sample>
+              <sample position="3">1.444444444444</sample>
+              <sample position="4">1.466666666667</sample>
+              <sample position="5">1.488888888889</sample>
+              <sample position="6">1.511111111111</sample>
+              <sample position="7">1.533333333333</sample>
+              <sample position="8">1.555555555556</sample>
+              <sample position="9">1.577777777778</sample>
+              <sample position="10">1.600000000000</sample>
             </samples>
           </designVariable>
           <designVariable uID="__desVar__/data_schema/aircraft/geometry/Lambda">
@@ -717,16 +717,16 @@
               </limitRange>
             </validRanges>
             <samples>
-              <sample position="1">40.0</sample>
-              <sample position="2">41.6666666667</sample>
-              <sample position="3">43.3333333333</sample>
-              <sample position="4">45.0</sample>
-              <sample position="5">46.6666666667</sample>
-              <sample position="6">48.3333333333</sample>
-              <sample position="7">50.0</sample>
-              <sample position="8">51.6666666667</sample>
-              <sample position="9">53.3333333333</sample>
-              <sample position="10">55.0</sample>
+              <sample position="1">40.000000000000</sample>
+              <sample position="2">41.666666666667</sample>
+              <sample position="3">43.333333333333</sample>
+              <sample position="4">45.000000000000</sample>
+              <sample position="5">46.666666666667</sample>
+              <sample position="6">48.333333333333</sample>
+              <sample position="7">50.000000000000</sample>
+              <sample position="8">51.666666666667</sample>
+              <sample position="9">53.333333333333</sample>
+              <sample position="10">55.000000000000</sample>
             </samples>
           </designVariable>
         </designVariables>
@@ -755,9 +755,6 @@
           <stateVariable uID="__statVar__/data_schema/mdo_data/objectives/R">
             <parameterUID>/data_schema/mdo_data/objectives/R</parameterUID>
           </stateVariable>
-          <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma5">
-            <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
-          </stateVariable>
           <stateVariable uID="__statVar__/data_schema/aircraft/weight/WE">
             <parameterUID>/data_schema/aircraft/weight/WE</parameterUID>
           </stateVariable>
@@ -767,6 +764,9 @@
           <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/propulsion/DT">
             <parameterUID>/data_schema/mdo_data/constraints/propulsion/DT</parameterUID>
           </stateVariable>
+          <stateVariable uID="__statVar__/data_schema/mdo_data/constraints/sigmas/sigma5">
+            <parameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</parameterUID>
+          </stateVariable>
         </stateVariables>
       </parameters>
       <executableBlocks>
@@ -1071,6 +1071,10 @@
           <fromParameterUID>/data_schema/aircraft/other/R</fromParameterUID>
           <toExecutableBlockUID>F[R]</toExecutableBlockUID>
         </edge>
+        <edge>
+          <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR</fromParameterUID>
+          <toExecutableBlockUID>DOE</toExecutableBlockUID>
+        </edge>
         <edge>
           <fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/other/L</fromParameterUID>
           <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
@@ -1119,10 +1123,6 @@
           <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/T</fromParameterUID>
           <toExecutableBlockUID>DOE</toExecutableBlockUID>
         </edge>
-        <edge>
-          <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</fromParameterUID>
-          <toExecutableBlockUID>DOE</toExecutableBlockUID>
-        </edge>
         <edge>
           <fromParameterUID>/data_schema/architectureNodes/initialGuessCouplingVariables/data_schemaCopy/aircraft/geometry/Theta</fromParameterUID>
           <toExecutableBlockUID>Aerodynamics[main][1][1.0]</toExecutableBlockUID>
@@ -1356,7 +1356,7 @@
           <toExecutableBlockUID>Structures[main][1][1.0]</toExecutableBlockUID>
         </edge>
         <edge>
-          <fromParameterUID>/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR</fromParameterUID>
+          <fromParameterUID>/data_schema/mdo_data/constraints/sigmas/sigma5</fromParameterUID>
           <toExecutableBlockUID>DOE</toExecutableBlockUID>
         </edge>
         <edge>
@@ -1612,6 +1612,10 @@
           <relatedParameterUID>/data_schema/reference/h</relatedParameterUID>
           <label>DOE_h_{inp}</label>
         </doeInputSampleList>
+        <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR">
+          <relatedParameterUID>/data_schema/aircraft/geometry/AR</relatedParameterUID>
+          <label>DOE_AR_{inp}</label>
+        </doeInputSampleList>
         <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/other/T">
           <relatedParameterUID>/data_schema/aircraft/other/T</relatedParameterUID>
           <label>DOE_T_{inp}</label>
@@ -1628,10 +1632,6 @@
           <relatedParameterUID>/data_schema/aircraft/geometry/section</relatedParameterUID>
           <label>DOE_section_{inp}</label>
         </doeInputSampleList>
-        <doeInputSampleList uID="/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/aircraft/geometry/AR">
-          <relatedParameterUID>/data_schema/aircraft/geometry/AR</relatedParameterUID>
-          <label>DOE_AR_{inp}</label>
-        </doeInputSampleList>
       </doeInputSampleLists>
       <doeOutputSampleLists>
         <doeOutputSampleList uID="/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/aircraft/weight/WE">
@@ -1697,19 +1697,19 @@
             <doeMethod>Custom design table</doeMethod>
             <doeTable>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/lambda">
-                <tableElement experimentID="0">0.1</tableElement>
+                <tableElement experimentID="0">0.100000000000</tableElement>
                 <tableElement experimentID="1">0.116666666667</tableElement>
                 <tableElement experimentID="2">0.133333333333</tableElement>
-                <tableElement experimentID="3">0.15</tableElement>
+                <tableElement experimentID="3">0.150000000000</tableElement>
                 <tableElement experimentID="4">0.166666666667</tableElement>
                 <tableElement experimentID="5">0.183333333333</tableElement>
-                <tableElement experimentID="6">0.2</tableElement>
+                <tableElement experimentID="6">0.200000000000</tableElement>
                 <tableElement experimentID="7">0.216666666667</tableElement>
                 <tableElement experimentID="8">0.233333333333</tableElement>
-                <tableElement experimentID="9">0.25</tableElement>
+                <tableElement experimentID="9">0.250000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/section">
-                <tableElement experimentID="0">0.75</tableElement>
+                <tableElement experimentID="0">0.750000000000</tableElement>
                 <tableElement experimentID="1">0.777777777778</tableElement>
                 <tableElement experimentID="2">0.805555555556</tableElement>
                 <tableElement experimentID="3">0.833333333333</tableElement>
@@ -1718,10 +1718,10 @@
                 <tableElement experimentID="6">0.916666666667</tableElement>
                 <tableElement experimentID="7">0.944444444444</tableElement>
                 <tableElement experimentID="8">0.972222222222</tableElement>
-                <tableElement experimentID="9">1.0</tableElement>
+                <tableElement experimentID="9">1.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/other/Cf">
-                <tableElement experimentID="0">0.75</tableElement>
+                <tableElement experimentID="0">0.750000000000</tableElement>
                 <tableElement experimentID="1">0.777777777778</tableElement>
                 <tableElement experimentID="2">0.805555555556</tableElement>
                 <tableElement experimentID="3">0.833333333333</tableElement>
@@ -1730,91 +1730,91 @@
                 <tableElement experimentID="6">0.916666666667</tableElement>
                 <tableElement experimentID="7">0.944444444444</tableElement>
                 <tableElement experimentID="8">0.972222222222</tableElement>
-                <tableElement experimentID="9">1.0</tableElement>
+                <tableElement experimentID="9">1.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/other/T">
-                <tableElement experimentID="0">0.1</tableElement>
-                <tableElement experimentID="1">0.15</tableElement>
-                <tableElement experimentID="2">0.2</tableElement>
-                <tableElement experimentID="3">0.25</tableElement>
-                <tableElement experimentID="4">0.3</tableElement>
-                <tableElement experimentID="5">0.35</tableElement>
-                <tableElement experimentID="6">0.4</tableElement>
-                <tableElement experimentID="7">0.45</tableElement>
-                <tableElement experimentID="8">0.5</tableElement>
-                <tableElement experimentID="9">0.55</tableElement>
+                <tableElement experimentID="0">0.100000000000</tableElement>
+                <tableElement experimentID="1">0.150000000000</tableElement>
+                <tableElement experimentID="2">0.200000000000</tableElement>
+                <tableElement experimentID="3">0.250000000000</tableElement>
+                <tableElement experimentID="4">0.300000000000</tableElement>
+                <tableElement experimentID="5">0.350000000000</tableElement>
+                <tableElement experimentID="6">0.400000000000</tableElement>
+                <tableElement experimentID="7">0.450000000000</tableElement>
+                <tableElement experimentID="8">0.500000000000</tableElement>
+                <tableElement experimentID="9">0.550000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/AR">
-                <tableElement experimentID="0">2.5</tableElement>
-                <tableElement experimentID="1">2.83333333333</tableElement>
-                <tableElement experimentID="2">3.16666666667</tableElement>
-                <tableElement experimentID="3">3.5</tableElement>
-                <tableElement experimentID="4">3.83333333333</tableElement>
-                <tableElement experimentID="5">4.16666666667</tableElement>
-                <tableElement experimentID="6">4.5</tableElement>
-                <tableElement experimentID="7">4.83333333333</tableElement>
-                <tableElement experimentID="8">5.16666666667</tableElement>
-                <tableElement experimentID="9">5.5</tableElement>
+                <tableElement experimentID="0">2.500000000000</tableElement>
+                <tableElement experimentID="1">2.833333333333</tableElement>
+                <tableElement experimentID="2">3.166666666667</tableElement>
+                <tableElement experimentID="3">3.500000000000</tableElement>
+                <tableElement experimentID="4">3.833333333333</tableElement>
+                <tableElement experimentID="5">4.166666666667</tableElement>
+                <tableElement experimentID="6">4.500000000000</tableElement>
+                <tableElement experimentID="7">4.833333333333</tableElement>
+                <tableElement experimentID="8">5.166666666667</tableElement>
+                <tableElement experimentID="9">5.500000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/Lambda">
-                <tableElement experimentID="0">40.0</tableElement>
-                <tableElement experimentID="1">41.6666666667</tableElement>
-                <tableElement experimentID="2">43.3333333333</tableElement>
-                <tableElement experimentID="3">45.0</tableElement>
-                <tableElement experimentID="4">46.6666666667</tableElement>
-                <tableElement experimentID="5">48.3333333333</tableElement>
-                <tableElement experimentID="6">50.0</tableElement>
-                <tableElement experimentID="7">51.6666666667</tableElement>
-                <tableElement experimentID="8">53.3333333333</tableElement>
-                <tableElement experimentID="9">55.0</tableElement>
+                <tableElement experimentID="0">40.000000000000</tableElement>
+                <tableElement experimentID="1">41.666666666667</tableElement>
+                <tableElement experimentID="2">43.333333333333</tableElement>
+                <tableElement experimentID="3">45.000000000000</tableElement>
+                <tableElement experimentID="4">46.666666666667</tableElement>
+                <tableElement experimentID="5">48.333333333333</tableElement>
+                <tableElement experimentID="6">50.000000000000</tableElement>
+                <tableElement experimentID="7">51.666666666667</tableElement>
+                <tableElement experimentID="8">53.333333333333</tableElement>
+                <tableElement experimentID="9">55.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/Sref">
-                <tableElement experimentID="0">500.0</tableElement>
-                <tableElement experimentID="1">555.555555556</tableElement>
-                <tableElement experimentID="2">611.111111111</tableElement>
-                <tableElement experimentID="3">666.666666667</tableElement>
-                <tableElement experimentID="4">722.222222222</tableElement>
-                <tableElement experimentID="5">777.777777778</tableElement>
-                <tableElement experimentID="6">833.333333333</tableElement>
-                <tableElement experimentID="7">888.888888889</tableElement>
-                <tableElement experimentID="8">944.444444444</tableElement>
-                <tableElement experimentID="9">1000.0</tableElement>
+                <tableElement experimentID="0">500.000000000000</tableElement>
+                <tableElement experimentID="1">555.555555555556</tableElement>
+                <tableElement experimentID="2">611.111111111111</tableElement>
+                <tableElement experimentID="3">666.666666666667</tableElement>
+                <tableElement experimentID="4">722.222222222222</tableElement>
+                <tableElement experimentID="5">777.777777777778</tableElement>
+                <tableElement experimentID="6">833.333333333333</tableElement>
+                <tableElement experimentID="7">888.888888888889</tableElement>
+                <tableElement experimentID="8">944.444444444444</tableElement>
+                <tableElement experimentID="9">1000.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/aircraft/geometry/tc">
-                <tableElement experimentID="0">0.01</tableElement>
-                <tableElement experimentID="1">0.0144444444444</tableElement>
-                <tableElement experimentID="2">0.0188888888889</tableElement>
-                <tableElement experimentID="3">0.0233333333333</tableElement>
-                <tableElement experimentID="4">0.0277777777778</tableElement>
-                <tableElement experimentID="5">0.0322222222222</tableElement>
-                <tableElement experimentID="6">0.0366666666667</tableElement>
-                <tableElement experimentID="7">0.0411111111111</tableElement>
-                <tableElement experimentID="8">0.0455555555556</tableElement>
-                <tableElement experimentID="9">0.05</tableElement>
+                <tableElement experimentID="0">0.010000000000</tableElement>
+                <tableElement experimentID="1">0.014444444444</tableElement>
+                <tableElement experimentID="2">0.018888888889</tableElement>
+                <tableElement experimentID="3">0.023333333333</tableElement>
+                <tableElement experimentID="4">0.027777777778</tableElement>
+                <tableElement experimentID="5">0.032222222222</tableElement>
+                <tableElement experimentID="6">0.036666666667</tableElement>
+                <tableElement experimentID="7">0.041111111111</tableElement>
+                <tableElement experimentID="8">0.045555555556</tableElement>
+                <tableElement experimentID="9">0.050000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/reference/h">
-                <tableElement experimentID="0">30000.0</tableElement>
-                <tableElement experimentID="1">31666.6666667</tableElement>
-                <tableElement experimentID="2">33333.3333333</tableElement>
-                <tableElement experimentID="3">35000.0</tableElement>
-                <tableElement experimentID="4">36666.6666667</tableElement>
-                <tableElement experimentID="5">38333.3333333</tableElement>
-                <tableElement experimentID="6">40000.0</tableElement>
-                <tableElement experimentID="7">41666.6666667</tableElement>
-                <tableElement experimentID="8">43333.3333333</tableElement>
-                <tableElement experimentID="9">45000.0</tableElement>
+                <tableElement experimentID="0">30000.000000000000</tableElement>
+                <tableElement experimentID="1">31666.666666666668</tableElement>
+                <tableElement experimentID="2">33333.333333333336</tableElement>
+                <tableElement experimentID="3">35000.000000000000</tableElement>
+                <tableElement experimentID="4">36666.666666666664</tableElement>
+                <tableElement experimentID="5">38333.333333333336</tableElement>
+                <tableElement experimentID="6">40000.000000000000</tableElement>
+                <tableElement experimentID="7">41666.666666666672</tableElement>
+                <tableElement experimentID="8">43333.333333333336</tableElement>
+                <tableElement experimentID="9">45000.000000000000</tableElement>
               </tableRow>
               <tableRow relatedParameterUID="/data_schema/reference/M">
-                <tableElement experimentID="0">1.4</tableElement>
-                <tableElement experimentID="1">1.42222222222</tableElement>
-                <tableElement experimentID="2">1.44444444444</tableElement>
-                <tableElement experimentID="3">1.46666666667</tableElement>
-                <tableElement experimentID="4">1.48888888889</tableElement>
-                <tableElement experimentID="5">1.51111111111</tableElement>
-                <tableElement experimentID="6">1.53333333333</tableElement>
-                <tableElement experimentID="7">1.55555555556</tableElement>
-                <tableElement experimentID="8">1.57777777778</tableElement>
-                <tableElement experimentID="9">1.6</tableElement>
+                <tableElement experimentID="0">1.400000000000</tableElement>
+                <tableElement experimentID="1">1.422222222222</tableElement>
+                <tableElement experimentID="2">1.444444444444</tableElement>
+                <tableElement experimentID="3">1.466666666667</tableElement>
+                <tableElement experimentID="4">1.488888888889</tableElement>
+                <tableElement experimentID="5">1.511111111111</tableElement>
+                <tableElement experimentID="6">1.533333333333</tableElement>
+                <tableElement experimentID="7">1.555555555556</tableElement>
+                <tableElement experimentID="8">1.577777777778</tableElement>
+                <tableElement experimentID="9">1.600000000000</tableElement>
               </tableRow>
             </doeTable>
           </settings>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-GS.xml b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-GS.xml
index 1c343f3a437731acb43bb2dea5cea4ff50ab4f35..22f0fe1a13249b003c3dd1cc7225c5cb292b82b5 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-GS.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-GS.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-21T15:55:30.252183</timestamp>
+    <timestamp>2018-03-24T09:14:31.749000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-21T15:55:30.252183</timestamp>
+        <timestamp>2018-03-24T09:14:31.749000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
diff --git a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-J.xml b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-J.xml
index 97dd25d01e7152ff6dc4284d4f99037737bd7fb7..428624edf3733e66e53ac66e2550543933cffb52 100644
--- a/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-J.xml
+++ b/examples/scripts/ssbj/CMDOWS/Mdao_unconverged-MDA-J.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Imco van Gent</creator>
     <description>Mdao CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-21T15:55:30.252183</timestamp>
+    <timestamp>2018-03-24T09:14:31.749000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a mdao data graph (MDG).</modification>
         <creator>Imco van Gent</creator>
-        <timestamp>2018-03-21T15:55:30.252183</timestamp>
+        <timestamp>2018-03-24T09:14:31.749000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
diff --git a/examples/scripts/ssbj/CMDOWS/RCG.xml b/examples/scripts/ssbj/CMDOWS/RCG.xml
index 8f6b5b0fafef4942681b8eb5cc0a4aa151818b51..c4a3bdff11eaf868561829672c7d7105ff33c4fc 100644
--- a/examples/scripts/ssbj/CMDOWS/RCG.xml
+++ b/examples/scripts/ssbj/CMDOWS/RCG.xml
@@ -3,14 +3,14 @@
   <header>
     <creator>Lukas Mueller</creator>
     <description>RCG CMDOWS file of the super-sonic business jet test case optimization problem</description>
-    <timestamp>2018-03-23T11:14:08.740222</timestamp>
+    <timestamp>2018-03-24T08:54:14.754000</timestamp>
     <fileVersion>0.1</fileVersion>
     <cmdowsVersion>0.7</cmdowsVersion>
     <updates>
       <update>
         <modification>KADMOS export of a repository connectivity graph (RCG).</modification>
         <creator>Lukas Mueller</creator>
-        <timestamp>2018-03-23T11:14:08.740222</timestamp>
+        <timestamp>2018-03-24T08:54:14.754000</timestamp>
         <fileVersion>0.1</fileVersion>
         <cmdowsVersion>0.7</cmdowsVersion>
       </update>
diff --git a/examples/scripts/ssbj/KDMS/FPG_MDO.kdms b/examples/scripts/ssbj/KDMS/FPG_MDO.kdms
index 6a2a3a48d25abadc31e1bed989b7c00816dc19fb..57cbfaf11103c12b6cd145139bed2cddb72b2f1c 100644
Binary files a/examples/scripts/ssbj/KDMS/FPG_MDO.kdms and b/examples/scripts/ssbj/KDMS/FPG_MDO.kdms differ
diff --git a/examples/scripts/ssbj/KDMS/Mdao_BLISS-2000.kdms b/examples/scripts/ssbj/KDMS/Mdao_BLISS-2000.kdms
index c772ec365a86999675f3fd82bea3d6047ed725a0..e2bfd83364741b8b3bacec2961f0ca1b0592c880 100644
--- a/examples/scripts/ssbj/KDMS/Mdao_BLISS-2000.kdms
+++ b/examples/scripts/ssbj/KDMS/Mdao_BLISS-2000.kdms
@@ -4,90 +4,101 @@ q)
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diff --git a/examples/scripts/ssbj/KDMS/Mdao_BLISS-2000_mpg.kdms b/examples/scripts/ssbj/KDMS/Mdao_BLISS-2000_mpg.kdms
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diff --git a/examples/scripts/ssbj/KDMS/Mdao_MDF-GS.kdms b/examples/scripts/ssbj/KDMS/Mdao_MDF-GS.kdms
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diff --git a/examples/scripts/ssbj/KDMS/Mdao_converged-DOE-GS-CT.kdms b/examples/scripts/ssbj/KDMS/Mdao_converged-DOE-GS-CT.kdms
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diff --git a/examples/scripts/ssbj/KDMS/Mdao_converged-DOE-GS-CT_mpg.kdms b/examples/scripts/ssbj/KDMS/Mdao_converged-DOE-GS-CT_mpg.kdms
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diff --git a/examples/scripts/ssbj/VISTOMS/VISTOMS.html b/examples/scripts/ssbj/VISTOMS/VISTOMS.html
index 6770e58866cc41611d44551def945378c98f1675..afcdd61500f18be66c02bec2a76c4c7cbc3f9f15 100644
--- a/examples/scripts/ssbj/VISTOMS/VISTOMS.html
+++ b/examples/scripts/ssbj/VISTOMS/VISTOMS.html
@@ -1879,7 +1879,7 @@ th, td {
 			}
 			
 			//@Imco: Here is the sellar problem example data
-			theData = {"graphs": [{"description": "Repository of the super-sonic business jet test case optimization problem", "problem_formulation": {}, "xdsm": {"nodes": [{"metadata": [{"name": "Coordinator"}, {"description": "Action block providing system inputs and collecting outputs."}, {"creator": "Imco van Gent"}], "type": "coordinator", "id": "id_Coordinator", "name": "Coordinator"}, {"metadata": [{"name": "Structures"}, {"mode": "main"}, {"version": "1.0"}, {"execution_info": null}, {"instance": "1"}, {"performance_info": null}, {"general_info": null}, {"projectSpecific": null}], "type": "rcganalysis", "id": "id_Structures", "name": "Structures"}, {"metadata": [{"name": "Aerodynamics"}, {"mode": "main"}, {"version": "1.0"}, {"execution_info": null}, {"instance": "1"}, {"performance_info": null}, {"general_info": null}, {"projectSpecific": null}], "type": "rcganalysis", "id": "id_Aerodynamics", "name": "Aerodynamics"}, {"metadata": [{"name": "Propulsion"}, {"mode": "main"}, {"version": "1.0"}, {"execution_info": null}, {"instance": "1"}, {"performance_info": null}, {"general_info": null}, {"projectSpecific": null}], "type": "rcganalysis", "id": "id_Propulsion", "name": "Propulsion"}, {"metadata": [{"name": "Performance"}, {"mode": "main"}, {"version": "1.0"}, {"execution_info": null}, {"instance": "1"}, {"performance_info": null}, {"general_info": null}, {"projectSpecific": null}], "type": "rcganalysis", "id": "id_Performance", "name": "Performance"}, {"metadata": [{"name": "C[sigmas]"}, {"instance": 1}], "type": "rcganalysis", "id": "id_Csigmas", "name": "Csigmas"}, {"metadata": [{"name": "C[Theta]"}, {"instance": 1}], "type": "rcganalysis", "id": "id_CTheta", "name": "CTheta"}, {"metadata": [{"name": "C[dpdx]"}, {"instance": 1}], "type": "rcganalysis", "id": "id_Cdpdx", "name": "Cdpdx"}, {"metadata": [{"name": "C[prop]"}, {"instance": 1}], "type": "rcganalysis", "id": "id_Cprop", "name": "Cprop"}, {"metadata": [{"name": "F[R]"}, {"instance": 1}], "type": "rcganalysis", "id": "id_FR", "name": "FR"}], "edges": [{"to": "id_FR", "from": "id_Performance", "name": "/data_schema/aircraft/other/R", "short_name": "1 couplings"}, {"to": "id_Aerodynamics", "from": "id_Coordinator", "name": "/data_schema/reference/h,/data_schema/aircraft/geometry/Sref,/data_schema/aircraft/geometry/AR,/data_schema/aircraft/other/Cf,/data_schema/aircraft/geometry/tc,/data_schema/reference/M,/data_schema/aircraft/geometry/Lambda,/data_schema/aircraft/other/CDmin", "short_name": "8 inputs"}, {"to": "id_Aerodynamics", "from": "id_Structures", "name": "/data_schema/aircraft/geometry/Theta,/data_schema/aircraft/weight/WT", "short_name": "2 inputs"}, {"to": "id_Aerodynamics", "from": "id_Propulsion", "name": "/data_schema/reference/ESF", "short_name": "1 inputs"}, {"to": "id_CTheta", "from": "id_Structures", "name": "/data_schema/aircraft/geometry/Theta", "short_name": "1 couplings"}, {"to": "id_Propulsion", "from": "id_Coordinator", "name": "/data_schema/reference/h,/data_schema/aircraft/weight/WBE,/data_schema/reference/M,/data_schema/aircraft/other/T", "short_name": "4 inputs"}, {"to": "id_Propulsion", "from": "id_Aerodynamics", "name": "/data_schema/aircraft/other/D", "short_name": "1 inputs"}, {"to": "id_Cprop", "from": "id_Propulsion", "name": "/data_schema/reference/ESF,/data_schema/reference/Temp,/data_schema/aircraft/other/DT", "short_name": "3 couplings"}, {"to": "id_Coordinator", "from": "id_FR", "name": "/data_schema/mdo_data/objectives/R", "short_name": "1 outputs"}, {"to": "id_Coordinator", "from": "id_CTheta", "name": "/data_schema/mdo_data/constraints/Theta", "short_name": "1 outputs"}, {"to": "id_Coordinator", "from": "id_Cdpdx", "name": "/data_schema/mdo_data/constraints/dpdx", "short_name": "1 outputs"}, {"to": "id_Coordinator", "from": "id_Cprop", "name": "/data_schema/mdo_data/constraints/propulsion/ESF,/data_schema/mdo_data/constraints/propulsion/Temp,/data_schema/mdo_data/constraints/propulsion/DT", "short_name": "3 outputs"}, {"to": "id_Coordinator", "from": "id_Csigmas", "name": "/data_schema/mdo_data/constraints/sigmas/sigma4,/data_schema/mdo_data/constraints/sigmas/sigma5,/data_schema/mdo_data/constraints/sigmas/sigma1,/data_schema/mdo_data/constraints/sigmas/sigma2,/data_schema/mdo_data/constraints/sigmas/sigma3", "short_name": "5 outputs"}, {"to": "id_Cdpdx", "from": "id_Aerodynamics", "name": "/data_schema/aircraft/other/dpdx", "short_name": "1 couplings"}, {"to": "id_Csigmas", "from": "id_Structures", "name": "/data_schema/aircraft/other/sigma5,/data_schema/aircraft/other/sigma4,/data_schema/aircraft/other/sigma3,/data_schema/aircraft/other/sigma2,/data_schema/aircraft/other/sigma1", "short_name": "5 couplings"}, {"to": "id_Performance", "from": "id_Coordinator", "name": "/data_schema/reference/h,/data_schema/reference/M", "short_name": "2 inputs"}, {"to": "id_Performance", "from": "id_Aerodynamics", "name": "/data_schema/aircraft/other/fin", "short_name": "1 inputs"}, {"to": "id_Performance", "from": "id_Structures", "name": "/data_schema/aircraft/weight/WT,/data_schema/aircraft/weight/WF", "short_name": "2 inputs"}, {"to": "id_Performance", "from": "id_Propulsion", "name": "/data_schema/aircraft/other/SFC", "short_name": "1 inputs"}, {"to": "id_Structures", "from": "id_Coordinator", "name": "/data_schema/aircraft/geometry/lambda,/data_schema/aircraft/geometry/Sref,/data_schema/aircraft/weight/WFO,/data_schema/aircraft/geometry/AR,/data_schema/aircraft/other/Nz,/data_schema/aircraft/geometry/tc,/data_schema/aircraft/geometry/Lambda,/data_schema/aircraft/weight/WO,/data_schema/aircraft/geometry/section", "short_name": "9 inputs"}, {"to": "id_Structures", "from": "id_Aerodynamics", "name": "/data_schema/aircraft/other/L", "short_name": "1 inputs"}, {"to": "id_Structures", "from": "id_Propulsion", "name": "/data_schema/aircraft/weight/WE", "short_name": "1 inputs"}], "workflow": []}, "edgeBundles": [{"input": ["Performance"], "pipeline_data": {"Performance": ["/data_schema/aircraft/other/R"]}, "name": "FR"}, {"input": ["Coordinator", "Structures", "Propulsion"], "pipeline_data": {"Coordinator": ["/data_schema/reference/h", "/data_schema/aircraft/geometry/Sref", "/data_schema/aircraft/geometry/AR", "/data_schema/aircraft/other/Cf", "/data_schema/aircraft/geometry/tc", "/data_schema/reference/M", "/data_schema/aircraft/geometry/Lambda", "/data_schema/aircraft/other/CDmin"], "Structures": ["/data_schema/aircraft/geometry/Theta", "/data_schema/aircraft/weight/WT"], "Propulsion": ["/data_schema/reference/ESF"]}, "name": "Aerodynamics"}, {"input": ["Structures"], "pipeline_data": {"Structures": ["/data_schema/aircraft/geometry/Theta"]}, "name": "CTheta"}, {"input": ["Coordinator", "Aerodynamics"], "pipeline_data": {"Coordinator": ["/data_schema/reference/h", "/data_schema/aircraft/weight/WBE", "/data_schema/reference/M", "/data_schema/aircraft/other/T"], "Aerodynamics": ["/data_schema/aircraft/other/D"]}, "name": "Propulsion"}, {"input": ["Propulsion"], "pipeline_data": {"Propulsion": ["/data_schema/reference/ESF", "/data_schema/reference/Temp", "/data_schema/aircraft/other/DT"]}, "name": "Cprop"}, {"input": ["F[R]", "C[Theta]", "C[dpdx]", "C[prop]", "C[sigmas]"], "pipeline_data": {"F[R]": ["/data_schema/mdo_data/objectives/R"], "C[Theta]": ["/data_schema/mdo_data/constraints/Theta"], "C[dpdx]": ["/data_schema/mdo_data/constraints/dpdx"], "C[prop]": ["/data_schema/mdo_data/constraints/propulsion/ESF", "/data_schema/mdo_data/constraints/propulsion/Temp", "/data_schema/mdo_data/constraints/propulsion/DT"], "C[sigmas]": ["/data_schema/mdo_data/constraints/sigmas/sigma4", "/data_schema/mdo_data/constraints/sigmas/sigma5", "/data_schema/mdo_data/constraints/sigmas/sigma1", "/data_schema/mdo_data/constraints/sigmas/sigma2", "/data_schema/mdo_data/constraints/sigmas/sigma3"]}, "name": "Coordinator"}, {"input": ["Aerodynamics"], "pipeline_data": {"Aerodynamics": ["/data_schema/aircraft/other/dpdx"]}, "name": "Cdpdx"}, {"input": ["Structures"], "pipeline_data": {"Structures": ["/data_schema/aircraft/other/sigma5", "/data_schema/aircraft/other/sigma4", "/data_schema/aircraft/other/sigma3", "/data_schema/aircraft/other/sigma2", "/data_schema/aircraft/other/sigma1"]}, "name": "Csigmas"}, {"input": ["Coordinator", "Aerodynamics", "Structures", "Propulsion"], "pipeline_data": {"Coordinator": ["/data_schema/reference/h", "/data_schema/reference/M"], "Aerodynamics": ["/data_schema/aircraft/other/fin"], "Structures": ["/data_schema/aircraft/weight/WT", "/data_schema/aircraft/weight/WF"], "Propulsion": ["/data_schema/aircraft/other/SFC"]}, "name": "Performance"}, {"input": ["Coordinator", "Aerodynamics", "Propulsion"], "pipeline_data": {"Coordinator": ["/data_schema/aircraft/geometry/lambda", "/data_schema/aircraft/geometry/Sref", "/data_schema/aircraft/weight/WFO", "/data_schema/aircraft/geometry/AR", "/data_schema/aircraft/other/Nz", "/data_schema/aircraft/geometry/tc", "/data_schema/aircraft/geometry/Lambda", "/data_schema/aircraft/weight/WO", "/data_schema/aircraft/geometry/section"], "Aerodynamics": ["/data_schema/aircraft/other/L"], "Propulsion": ["/data_schema/aircraft/weight/WE"]}, "name": "Structures"}], "organization": null, "variableSchemes": {"catschema_sysLev": {"name": "systemVariables", "children": [{"level": 1, "type": "variable", "children": [{"level": 2, "type": "variable", "children": [{"level": 3, "type": "variable", "children": [{"level": 4, "type": "variable", "children": [{"type": "variable", "name": "sigma1", "level": 5}, {"type": "variable", "name": "sigma5", "level": 5}, {"type": "variable", "name": "sigma4", "level": 5}, {"type": "variable", "name": "sigma3", "level": 5}, {"type": "variable", "name": "sigma2", "level": 5}, {"type": "variable", "name": "DT", "level": 5}, {"type": "variable", "name": "dpdx", "level": 5}, {"type": "variable", "name": "R", "level": 5}, {"type": "variable", "name": "SFC", "level": 5}, {"type": 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{"type": "variable", "name": "CDmin", "level": 5}, {"type": "variable", "name": "T", "level": 5}], "name": "other"}, {"level": 4, "type": "variable", "children": [{"type": "variable", "name": "WO", "level": 5}, {"type": "variable", "name": "WFO", "level": 5}, {"type": "variable", "name": "WBE", "level": 5}], "name": "weight"}, {"level": 4, "type": "variable", "children": [{"type": "variable", "name": "lambda", "level": 5}, {"type": "variable", "name": "section", "level": 5}, {"type": "variable", "name": "AR", "level": 5}, {"type": "variable", "name": "Lambda", "level": 5}, {"type": "variable", "name": "Sref", "level": 5}, {"type": "variable", "name": "tc", "level": 5}], "name": "geometry"}], "name": "aircraft"}, {"level": 3, "type": "variable", "children": [{"type": "variable", "name": "h", "level": 4}, {"type": "variable", "name": "M", "level": 4}], "name": "reference"}], "name": "data_schema"}], "name": "inputs"}, {"level": 1, "type": "variable", "children": [{"level": 2, "type": "variable", "children": [{"level": 3, "type": "variable", "children": [{"level": 4, "type": "variable", "children": [{"type": "variable", "name": "dpdx", "level": 5}, {"type": "variable", "name": "Theta", "level": 5}, {"level": 5, "type": "variable", "children": [{"type": "variable", "name": "Temp", "level": 6}, {"type": "variable", "name": "ESF", "level": 6}, {"type": "variable", "name": "DT", "level": 6}], "name": "propulsion"}, {"level": 5, "type": "variable", "children": [{"type": "variable", "name": "sigma4", "level": 6}, {"type": "variable", "name": "sigma1", "level": 6}, {"type": "variable", "name": "sigma2", "level": 6}, {"type": "variable", "name": "sigma3", "level": 6}, {"type": "variable", "name": "sigma5", "level": 6}], "name": "sigmas"}], "name": "constraints"}, {"level": 4, "type": "variable", "children": [{"type": "variable", "name": "R", "level": 5}], "name": "objectives"}], "name": "mdo_data"}], "name": "data_schema"}], "name": "outputs"}]}, "catschema_nodeLev": 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"/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/distributedArchitectures/group2/couplingWeights/w2,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/distributedArchitectures/group2/couplingWeights/w0,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/distributedArchitectures/group2/couplingWeights/w1,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/architectureNodes/copyDesignVariables/data_schemaCopy/reference/h__i2,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/architectureNodes/copyDesignVariables/data_schemaCopy/reference/M__i2,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/D__i2", "short_name": "6 couplings"}, {"to": "id_Sub-SM-builder-2", "from": "id_Sub-DOE-2", "name": "/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/aircraft/weight/WE,/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/reference/ESF,/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalDesignVariables/data_schemaCopy/aircraft/other/T,/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/aircraft/other/SFC", "short_name": "4 couplings"}, {"to": "id_Sub-SM-builder-0", "from": "id_Sub-DOE-0", "name": "/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/aircraft/weight/WT,/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalDesignVariables/data_schemaCopy/aircraft/geometry/section,/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalDesignVariables/data_schemaCopy/aircraft/geometry/lambda,/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/aircraft/weight/WF,/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/aircraft/geometry/Theta", "short_name": "5 couplings"}, {"to": "id_Sub-SM-builder-0", "from": "id_Sub-SM-bounds-0", "name": "/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/Lambda,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/Sref,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/distributedArchitectures/group0/couplingWeights/w0,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/AR,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/distributedArchitectures/group0/couplingWeights/w2,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/distributedArchitectures/group0/couplingWeights/w1,/data_schema/architectureNodes/doeInputSampleLists/data_schemaCopy/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/tc", "short_name": "9 couplings"}, {"to": "id_Sub-SM-builder-1", "from": "id_Sub-DOE-1", "name": "/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/aircraft/other/L,/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalDesignVariables/data_schemaCopy/aircraft/other/Cf,/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/aircraft/other/fin,/data_schema/architectureNodes/doeOutputSampleLists/data_schemaCopy/architectureNodes/finalOutputVariables/data_schemaCopy/aircraft/other/D", "short_name": "4 couplings"}, {"to": "id_Sub-SM-builder-1", "from": "id_Sub-SM-bounds-1", "name": 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"short_name": "12 couplings"}, {"to": "id_WCF2", "from": "id_Propulsion", "name": "/data_schema/reference/ESF,/data_schema/aircraft/weight/WE,/data_schema/aircraft/other/SFC", "short_name": "3 couplings"}, {"to": "id_WCF2", "from": "id_Sub-DOE-2", "name": "/data_schema/distributedArchitectures/group2/couplingWeights/w2,/data_schema/distributedArchitectures/group2/couplingWeights/w1,/data_schema/distributedArchitectures/group2/couplingWeights/w0", "short_name": "3 couplings"}, {"to": "id_Sub-Surrogate-Model-1", "from": "id_Sys-Optimizer", "name": "/data_schema/distributedArchitectures/group1/couplingWeights/w1__i2,/data_schema/reference/h,/data_schema/aircraft/geometry/Sref,/data_schema/aircraft/geometry/AR,/data_schema/distributedArchitectures/group1/couplingWeights/w2__i2,/data_schema/aircraft/geometry/tc,/data_schema/reference/M,/data_schema/aircraft/geometry/Lambda,/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WT,/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/geometry/Theta,/data_schema/distributedArchitectures/group1/couplingWeights/w0__i2,/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF__i2", "short_name": "12 couplings"}, {"to": "id_Sub-Surrogate-Model-1", "from": "id_Sub-SM-builder-1", "name": "//surrogateModels/SubSMB1/definition", "short_name": "1 couplings"}, {"to": "id_Sub-Surrogate-Model-0", "from": "id_Sys-Optimizer", "name": "/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE__i2,/data_schema/aircraft/geometry/Sref,/data_schema/aircraft/geometry/AR,/data_schema/distributedArchitectures/group0/couplingWeights/w2__i2,/data_schema/aircraft/geometry/tc,/data_schema/aircraft/geometry/Lambda,/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L__i2,/data_schema/distributedArchitectures/group0/couplingWeights/w1__i2,/data_schema/distributedArchitectures/group0/couplingWeights/w0__i2", "short_name": "9 couplings"}, {"to": "id_Sub-Surrogate-Model-0", "from": "id_Sub-SM-builder-0", "name": "//surrogateModels/SubSMB0/definition", "short_name": "1 couplings"}, {"to": "id_Sub-Surrogate-Model-2", "from": "id_Sub-SM-builder-2", "name": "//surrogateModels/SubSMB2/definition", "short_name": "1 couplings"}, {"to": "id_Sub-Surrogate-Model-2", "from": "id_Sys-Optimizer", "name": "/data_schema/distributedArchitectures/group2/couplingWeights/w0__i2,/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/D,/data_schema/reference/h,/data_schema/distributedArchitectures/group2/couplingWeights/w1__i2,/data_schema/reference/M,/data_schema/distributedArchitectures/group2/couplingWeights/w2__i2", "short_name": "6 couplings"}, {"to": "id_Cdpdx", "from": "id_Aerodynamics", "name": "/data_schema/aircraft/other/dpdx", "short_name": "1 couplings"}, {"to": "id_Gc", "from": "id_Sub-Surrogate-Model-1", "name": "/data_schema/architectureNodes/surrogateModelApproximates/data_schemaCopy/aircraft/other/L,/data_schema/architectureNodes/surrogateModelApproximates/data_schemaCopy/aircraft/other/D", "short_name": "2 couplings"}, {"to": "id_Gc", "from": "id_Sub-Surrogate-Model-0", "name": "/data_schema/architectureNodes/surrogateModelApproximates/data_schemaCopy/aircraft/geometry/Theta,/data_schema/architectureNodes/surrogateModelApproximates/data_schemaCopy/aircraft/weight/WT", "short_name": "2 couplings"}, {"to": "id_Gc", "from": "id_Sub-Surrogate-Model-2", "name": "/data_schema/architectureNodes/surrogateModelApproximates/data_schemaCopy/aircraft/weight/WE,/data_schema/architectureNodes/surrogateModelApproximates/data_schemaCopy/reference/ESF", "short_name": "2 couplings"}, {"to": "id_Gc", "from": "id_Sys-Optimizer", "name": "/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WE__i2,/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/D,/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/other/L__i2,/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/geometry/Theta,/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WT,/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF__i2", "short_name": "6 couplings"}, {"to": "id_Aerodynamics", "from": "id_Coordinator", "name": "/data_schema/aircraft/other/CDmin", "short_name": "1 inputs"}, {"to": "id_Aerodynamics", "from": "id_Sub-DOE-1", "name": "/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/weight/WT__i2,/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/tc__i2,/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/AR__i2,/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/reference/h,/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/reference/M,/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/reference/ESF,/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/Sref__i2,/data_schema/architectureNodes/copyDesignVariables/data_schemaCopy/aircraft/geometry/Lambda__i2,/data_schema/architectureNodes/couplingCopyVariables/data_schemaCopy/aircraft/geometry/Theta__i2", "short_name": "9 inputs"}, {"to": "id_Aerodynamics", "from": "id_Sub-Optimizer-1", "name": "/data_schema/aircraft/other/Cf", "short_name": "1 inputs"}, {"to": "id_Coordinator", "from": "id_FR", "name": "/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/objectives/R", "short_name": "1 outputs"}, {"to": "id_Coordinator", "from": "id_Sub-Surrogate-Model-2", "name": "/data_schema/architectureNodes/surrogateModelApproximates/data_schemaCopy/aircraft/other/T", "short_name": "1 outputs"}, {"to": "id_Coordinator", "from": "id_Sys-Optimizer", "name": "/data_schema/architectureNodes/finalDesignVariables/data_schemaCopy/aircraft/geometry/Lambda,/data_schema/architectureNodes/finalDesignVariables/data_schemaCopy/aircraft/geometry/tc,/data_schema/architectureNodes/finalDesignVariables/data_schemaCopy/aircraft/geometry/Sref,/data_schema/architectureNodes/finalDesignVariables/data_schemaCopy/reference/h,/data_schema/architectureNodes/finalDesignVariables/data_schemaCopy/aircraft/geometry/AR,/data_schema/architectureNodes/finalDesignVariables/data_schemaCopy/reference/M", "short_name": "6 outputs"}, {"to": "id_Coordinator", "from": "id_WCF1", "name": 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"/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/sigmas/sigma5,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/sigmas/sigma4,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/sigmas/sigma1,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/sigmas/sigma3,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/sigmas/sigma2", "short_name": "5 outputs"}, {"to": "id_Coordinator", "from": "id_Gc", "name": "/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/systemLevel/consistencyConstraints/gc0,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/systemLevel/consistencyConstraints/gc1,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/systemLevel/consistencyConstraints/gc2,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/systemLevel/consistencyConstraints/gc3,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/systemLevel/consistencyConstraints/gc4,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/systemLevel/consistencyConstraints/gc5", "short_name": "6 outputs"}, {"to": "id_Coordinator", "from": "id_WCF2", "name": "/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/distributedArchitectures/group2/objective", "short_name": "1 outputs"}, {"to": "id_Sub-SM-bounds-1", "from": "id_Coordinator", "name": 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"name": "/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/objectives/R", "short_name": "1 outputs"}, {"to": "id_Coordinator", "from": "id_Sub-Surrogate-Model-2", "name": "/data_schema/architectureNodes/surrogateModelApproximates/data_schemaCopy/aircraft/other/T", "short_name": "1 outputs"}, {"to": "id_Coordinator", "from": "id_Sys-Optimizer", "name": "/data_schema/architectureNodes/finalDesignVariables/data_schemaCopy/aircraft/geometry/Lambda,/data_schema/architectureNodes/finalDesignVariables/data_schemaCopy/aircraft/geometry/tc,/data_schema/architectureNodes/finalDesignVariables/data_schemaCopy/aircraft/geometry/Sref,/data_schema/architectureNodes/finalDesignVariables/data_schemaCopy/reference/h,/data_schema/architectureNodes/finalDesignVariables/data_schemaCopy/aircraft/geometry/AR,/data_schema/architectureNodes/finalDesignVariables/data_schemaCopy/reference/M", "short_name": "6 outputs"}, {"to": "id_Coordinator", "from": "id_WCF1", "name": 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"/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/sigmas/sigma5,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/sigmas/sigma4,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/sigmas/sigma1,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/sigmas/sigma3,/data_schema/architectureNodes/finalOutputVariables/data_schemaCopy/mdo_data/constraints/sigmas/sigma2", "short_name": "5 outputs"}, {"to": "id_Coordinator", "from": "id_Gc", "name": 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{"level": 2, "type": "variable", "name": "M", "value": "unknown", "dimension": null}, {"level": 2, "type": "variable", "name": "Temp", "value": "unknown", "dimension": null}], "name": "reference"}]}}, "id": "29", "name": "XDSM - converged-DOE-GS-MC - Mdao"}], "categories": [{"name": "schema", "description": "schema"}, {"name": "catschema_nodeLev", "description": "node levels"}, {"name": "catschema_funLev", "description": "function levels"}, {"name": "catschema_roleLev", "description": "role levels"}, {"name": "catschema_sysLev", "description": "system levels"}]}
 			function loadAllData(data)
 			{
 				makeKadmosMenu(data);
diff --git a/kadmos/cmdows/schemas/0.8/cmdows.xsd b/kadmos/cmdows/schemas/0.8/cmdows.xsd
index 6983e77b5942cdaac984312edc7a5e57da952fb4..32ae7cff74a7cf99353f386bb4454099c8baa655 100644
--- a/kadmos/cmdows/schemas/0.8/cmdows.xsd
+++ b/kadmos/cmdows/schemas/0.8/cmdows.xsd
@@ -588,8 +588,8 @@
 																								<xs:element name="sample" maxOccurs="unbounded">
 																									<xs:complexType>
 																										<xs:simpleContent>
-																											<xs:extension base="xs:string">
-																												<xs:attribute name="position" type="xs:int"/>
+																											<xs:extension base="xs:decimal">
+																												<xs:attribute name="position" type="xs:string"/>
 																											</xs:extension>
 																										</xs:simpleContent>
 																									</xs:complexType>
@@ -993,7 +993,7 @@
 																											<xs:element name="tableElement" maxOccurs="unbounded">
 																												<xs:complexType>
 																													<xs:simpleContent>
-																														<xs:extension base="xs:float">
+																														<xs:extension base="xs:decimal">
 																															<xs:attribute name="experimentID" type="xs:string"/>
 																														</xs:extension>
 																													</xs:simpleContent>
@@ -1007,6 +1007,8 @@
 																						</xs:complexType>
 																					</xs:element>
 																					<xs:element name="doeMethod" type="xs:string"/>
+																					<xs:element name="doeRuns" type="xs:integer"/>
+																					<xs:element name="doeSeed" type="xs:integer"/>
 																				</xs:all>
 																			</xs:complexType>
 																		</xs:element>
@@ -1031,24 +1033,24 @@
 												</xs:sequence>
 											</xs:complexType>
 										</xs:element>
-										<xs:element name="surrogateModels">
+										<xs:element name="surrogateModels" minOccurs="0">
 											<xs:complexType>
 												<xs:sequence>
-													<xs:element name="surrogateModel" type="simpleArchitectureElementsBlockType" maxOccurs="unbounded"/>
+													<xs:element name="surrogateModel" type="simpleArchitectureElementsRelatedBlockType" maxOccurs="unbounded"/>
 												</xs:sequence>
 											</xs:complexType>
 										</xs:element>
 										<xs:element name="boundaryDeterminators" minOccurs="0">
 											<xs:complexType>
 												<xs:sequence>
-													<xs:element name="boundaryDeterminator" type="simpleArchitectureElementsBlockType" maxOccurs="unbounded"/>
+													<xs:element name="boundaryDeterminator" type="simpleArchitectureElementsRelatedBlockType" maxOccurs="unbounded"/>
 												</xs:sequence>
 											</xs:complexType>
 										</xs:element>
 										<xs:element name="surrogateModelBuilders" minOccurs="0">
 											<xs:complexType>
 												<xs:sequence>
-													<xs:element name="surrogateModelBuilder" type="simpleArchitectureElementsBlockType" maxOccurs="unbounded"/>
+													<xs:element name="surrogateModelBuilder" type="simpleArchitectureElementsRelatedBlockType" maxOccurs="unbounded"/>
 												</xs:sequence>
 											</xs:complexType>
 										</xs:element>
@@ -1221,8 +1223,22 @@
 	</xs:complexType>
 	<xs:complexType name="simpleArchitectureElementsBlockType">
 		<xs:sequence>
-			<xs:element name="label" type="xs:string"/>
-			<xs:element name="settings" type="xs:string" minOccurs="0"/>
+			<xs:element name="label" type="xs:string" />
+			<xs:element name="settings" minOccurs="0">
+				<xs:complexType>
+					<xs:sequence>
+						<xs:element name="lastIterationsToConsider" type="xs:decimal"/>
+						<xs:element name="maximumIterations" type="xs:decimal"/>
+						<xs:element name="algorithm" type="xs:string"/>
+						<xs:element name="applyScaling" type="xs:boolean"/>
+						<xs:element name="maximumFunctionEvaluations" type="xs:decimal"/>
+						<xs:element name="constraintTolerance" type="xs:decimal"/>
+						<xs:element name="convergenceTolerance" type="xs:decimal"/>
+						<xs:element name="convergenceToleranceRelative" type="xs:decimal"/>
+						<xs:element name="convergenceToleranceAbsolute" type="xs:decimal"/>
+					</xs:sequence>
+				</xs:complexType>
+			</xs:element>
 		</xs:sequence>
 		<xs:attribute name="uID" type="xs:string"/>
 	</xs:complexType>
diff --git a/kadmos/graph/graph_data.py b/kadmos/graph/graph_data.py
index c8dc9270ec9816323d19735563600926427a4576..11a5f2ccdd471d7a1fb0a6cb4c41ea855714b98b 100644
--- a/kadmos/graph/graph_data.py
+++ b/kadmos/graph/graph_data.py
@@ -14,6 +14,7 @@ import numpy as np
 
 from types import NoneType
 
+
 from kadmos.utilities.strings import get_correctly_extended_latex_label
 from ..utilities import prompting
 from ..utilities import printing
@@ -93,7 +94,7 @@ class DataGraph(KadmosGraph):
                         cmdows_samples = cmdows_problem_role.add('samples')
                         if self.node[graph_problem_role].get(cmdows_problem_role_attr) is not None:
                             for idx, itm in enumerate(self.node[graph_problem_role].get(cmdows_problem_role_attr)):
-                                cmdows_samples.add('sample', itm, attrib={'position': str(idx + 1)})
+                                cmdows_samples.add('sample', format(itm, '.12f'), attrib={'position': str(idx + 1)})
                     else:
                         cmdows_problem_role.add(self.CMDOWS_ATTRIBUTE_DICT[cmdows_problem_role_attr],
                                                 self.node[graph_problem_role].get(cmdows_problem_role_attr),
@@ -124,8 +125,7 @@ class DataGraph(KadmosGraph):
         if cmdows_problem_formulation is not None:
             graph_problem_form['mdao_architecture'] = cmdows_problem_formulation.findtext('mdaoArchitecture')
             graph_problem_form['convergence_type'] = cmdows_problem_formulation.findtext('convergerType')
-            cmdows_executable_blocks = cmdows_problem_formulation.find('executableBlocksOrder').findall(
-                'executableBlock')
+            cmdows_executable_blocks = cmdows_problem_formulation.find('executableBlocksOrder').findall('executableBlock')
             cmdows_executable_blocks_order = [None] * len(list(cmdows_executable_blocks))
             for cmdows_executable_block in cmdows_executable_blocks:
                 cmdows_executable_blocks_order[int(cmdows_executable_block.get('position')
@@ -2522,6 +2522,7 @@ class FundamentalProblemGraph(DataGraph, KeChainMixin):
         # Return
         return category_check, i
 
+
     # ---------------------------------------------------------------------------------------------------------------- #
     #                                          GRAPH SPECIFIC METHODS                                                  #
     # ---------------------------------------------------------------------------------------------------------------- #
@@ -4135,7 +4136,7 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
                             for graph_row_index, graph_row in enumerate(graph_settings.get('doe_table_order')):
                                 cmdows_row = cmdows_table.add('tableRow', attrib={'relatedParameterUID': str(graph_row)})
                                 for graph_element_index, graph_element in enumerate(graph_settings.get('doe_table')):
-                                    cmdows_row.add('tableElement', graph_element[graph_row_index],
+                                    cmdows_row.add('tableElement', str(format(float(graph_element[graph_row_index]),'.12f')),
                                                    attrib={'experimentID': str(graph_element_index)})
                         graph_des_vars = [{'designVariableUID': self.PROBLEM_ROLES_VAR_SUFFIXES[0] + var} for var in
                                           self.node[graph_node].get('design_variables')]
@@ -4190,6 +4191,29 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
                         cmdows_des_vars = cmdows_single_architecture_exe_block.findall('designVariables/designVariable')
                         graph_des_vars = [var.findtext('designVariableUID')[10:] for var in list(cmdows_des_vars)]
                         self.node[cmdows_uid]['design_variables'] = graph_des_vars
+                    if role == 'converger' or role == 'optimizer':
+                        if 'settings' not in self.node[cmdows_uid] or self.node[cmdows_uid]['settings'] is None:
+                            self.node[cmdows_uid]['settings'] = {}
+                        if role == 'converger':
+                            setting_options = {'last_iterations_to_consider':'lastIterationsToConsider',
+                                               'maximum_iterations':'maximumIterations',
+                                               'convergence_tolerance_relative':'convergenceToleranceRelative',
+                                               'convergence_tolerance_absolute':'convergenceToleranceAbsolute'}
+                        else:
+                            setting_options = {'maximum_iterations':'maximumIterations',
+                                               'algorithm':'algorithm',
+                                               'apply_scaling':'applyScaling',
+                                               'maximum_function_evaluations':'maximumFunctionEvaluations',
+                                               'constraint_tolerance':'constraintTolerance',
+                                               'convergence_tolerance':'convergenceTolerance'}
+                        for setting_option in setting_options:
+                            if setting_option == 'apply_scaling':
+                                bool_options = {'true':True,'false':False}
+                                self.node[cmdows_uid]['settings'][setting_option] = \
+                                    bool_options[cmdows_single_architecture_exe_block.findtext('settings/'+setting_options[setting_option])]
+                            else:
+                                self.node[cmdows_uid]['settings'][setting_option] = \
+                                    cmdows_single_architecture_exe_block.findtext('settings/'+setting_options[setting_option])
                     if role == 'optimizer':
                         cmdows_des_vars = cmdows_single_architecture_exe_block.findall('objectiveVariables/objectiveVariable')
                         graph_des_vars = [var.findtext('objectiveVariableUID')[10:] for var in list(cmdows_des_vars)]
@@ -4205,13 +4229,18 @@ class MdaoDataGraph(DataGraph, MdaoMixin):
                             def get_experiment_id(elem):
                                 return float(elem.get('experimentID'))
                             elements = sorted(cmdows_row, key=get_experiment_id)
-                            graph_table.append([element.findasttext() for element in elements])
+                            entry = []
+                            for element in elements:
+                                entry.append(format(element.findasttext(),'.12f'))
+                            graph_table.append(entry)
                         graph_table = map(list, zip(*graph_table))
                         if 'settings' not in self.node[cmdows_uid] or self.node[cmdows_uid]['settings'] is None:
                             self.node[cmdows_uid]['settings'] = {}
                         self.node[cmdows_uid]['settings']['doe_table_order'] = graph_rows
                         self.node[cmdows_uid]['settings']['doe_table'] = graph_table
                         self.node[cmdows_uid]['settings']['doe_method'] = cmdows_single_architecture_exe_block.findtext('settings/doeMethod')
+                        self.node[cmdows_uid]['settings']['doe_runs'] = cmdows_single_architecture_exe_block.findtext('settings/doeRuns')
+                        self.node[cmdows_uid]['settings']['doe_seed'] = cmdows_single_architecture_exe_block.findtext('settings/doeSeed')
 
                 else:
                     for role in self.ARCHITECTURE_ROLES_FUNS:
diff --git a/kadmos/utilities/xmls.py b/kadmos/utilities/xmls.py
index 41b465fd053c66a9ca1514cfe0b247be0af2ff6f..1b7d9b5f452ee4bf723f8df79ede40c28a6f7e63 100644
--- a/kadmos/utilities/xmls.py
+++ b/kadmos/utilities/xmls.py
@@ -226,9 +226,13 @@ class ExtendedElement(etree.ElementBase):
         elif type(value) == list:
             child = self._add_array(tag, value, attrib, camel_case_conversion, **extra)
 
+        elif type(value) == bool:
+            child = self._add_bool(tag, value, attrib, **extra)
+
         else:
             child = self._add_element(tag, value, attrib, **extra)
 
+
         return child
 
     def _add_dictionary(self, tag, dictionary, attrib=None, camel_case_conversion=False, **extra):
@@ -288,6 +292,28 @@ class ExtendedElement(etree.ElementBase):
 
         return child
 
+    def _add_bool(self, tag, bool, attrib=None, **extra):
+        """Method to add a new sub element to the element based on a boolean
+
+        :param tag: The sub element tag
+        :type tag: str
+        :param bool: The boolean
+        :type bool: bool
+        :param attrib: An optional dictionary containing sub element attributes
+        :param extra: Additional sub element attributes given as keyword arguments
+        :return: An element instance
+        :rtype: Element
+        """
+
+        child = SubElement(self, tag, attrib, **extra)
+
+        if bool:
+            child.text = 'true'
+        else:
+            child.text = 'false'
+
+        return child
+
     def _add_element(self, tag, element, attrib=None, **extra):
         """Method to add a new sub element to the element based on a simple string, float, int, etx.