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Created with Raphaël 2.2.013Dec1211108765432130Nov2928272625242322212019161514131211109767652130Oct28272625242322201918171615121110985432Fix catkin/ROS build paths.nxphlite-v3:SDHC setting is for EMI issue with GPS and FCC (#11029)rcS,rc.serial.jinja:ensure proper unset hygienev1.9.0-alphav1.9.0-alphacommander run preflight immediately (#11018)integrationtestsmaneuver name is given as a command line argument to the test_runner shell scriptmaneuver name is now also read from yaml fileyaml file with parameters for integrationtests. Deselected tests do not get executedrun_tests: do not start px4-shellMove common shmem parameter declarations to shmem.h.Use correct path when looking up df wrapper.Fix some dynamic linking errors.Fix paths in snapdragon upload code.Make name mangling type consistent.Improve forcefail/terminatefail docsFlightTask: use convetion for definition of the landing gear default valueFlightTask Manual: Gear react only on switch changes and not statesFlightTAsk AutoMapper: Adapt to new messageFlightTask Auto: Adapt to new message and rename variableposition_setpoint: Change deploy gear to landing gearmc_pos_ctrl: Remove gear intialisationFlightTask AutoMapper: Use deploy gear informationFlightTask Auto: Save deploy gear informationFlightTask: Add initialisation of the landing gearvehicle constraints: remove landing gearFlightTasks: Add interface for landing gearFlightTask: Add interface for landing gearRename the invered state and make namespace more clearmsg landing_gear: change type to int8mc_pos_ctrl: Replace landing gear logicremove the landing gear from the attitude setpointmc_att_control: don't generate attitude setpoint for tailsitterspr-tecs_front_t…pr-tecs_front_transsupport for pitch control via TECS during front transitionsupdated eclcommander: fix orbit failsafes for data link & rc lossmc_pos_control: let orbit task do its workcommander: add orbit state handlingmsg: add orbit main and navigation statemc_att_control: don't generate attitude setpoint for tailsitterspr-tailsitterpr-tailsittermav_cmd_do_reposition now obeys the ground speed argument
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