- Oct 17, 2018
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Paul Riseborough authored
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Paul Riseborough authored
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Paul Riseborough authored
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Paul Riseborough authored
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- Oct 16, 2018
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Dennis Mannhart authored
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Dennis Mannhart authored
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Dennis Mannhart authored
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Dennis Mannhart authored
mc_pos_control_main smooth takeoff: enable position-xy/yaw control once above 0.5m from takeoff reference
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Dennis Mannhart authored
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Dennis Mannhart authored
just keep thrust vector pointing upward
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Dennis Mannhart authored
smooth-takeoff. This is only required if someone writes a FlightTask where both position and velocity setpoints are finite
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PX4 Build Bot authored
- libuavcan in PX4/Firmware (8958b42dada1e14f27c287a59b51ff26e90486a1): https://github.com/UAVCAN/libuavcan/commit/479d144ded9d5d16e234121ef9511b9ca9dfdac5 - libuavcan current upstream: https://github.com/UAVCAN/libuavcan/commit/6174b8c10a2dbf47076ca7a7b5820a4c36c8a988 - Changes: https://github.com/UAVCAN/libuavcan/compare/479d144ded9d5d16e234121ef9511b9ca9dfdac5...6174b8c10a2dbf47076ca7a7b5820a4c36c8a988 6174b8c 2018-10-06 Pavel Kirienko - Link to the new forum
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- Oct 10, 2018
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Dennis Mannhart authored
vehicle state.
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Dennis Mannhart authored
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Dennis Mannhart authored
refactor use_obstacle_avoidance method
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- Oct 09, 2018
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Martina authored
acceptance radius from the paramters and overwrite it if the mission item has set acceptance radius
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Beat Küng authored
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Beat Küng authored
The hover thrust param also changed the thrust scaling in Stabilized mode. However if the hover thrust is very low (e.g. below 20%), the throttle stick input becomes very distorted.
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Beat Küng authored
- no airframe changes the default - it does not make much sense to be able to configure the 0.1 threshold but the 0.3 threshold for ground contact detection cannot be configured.
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bresch authored
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- Oct 08, 2018
- Oct 04, 2018
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Beat Küng authored
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Julian Oes authored
This fixes the build with Python 3.7.
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- Oct 03, 2018
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Beat Küng authored
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David Sidrane authored
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- Oct 02, 2018
- Oct 01, 2018
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Matthias Grob authored
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- Sep 29, 2018
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Paul Riseborough authored
A filtered update update interval is calculated for each receiver. If dissimilar interval data is detected, blending occurs when data is received from the slower of the receivers. If similar interval data is detected, blending occurs when receiver data with similar time stamps is available. If no data is received from either receiver for longer than 300msec, then no blending will be performed and the most recent data will be used instead.
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Beat Küng authored
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Beat Küng authored
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Beat Küng authored
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Beat Küng authored
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Beat Küng authored
- previously it was possible to get a Position Control rejected message without further advice what was actually wrong. So now we report warnings even if gps is not required for arming (which could be annoying too...). - the GPS failure message was very generic, making it hard to debug the cause. Now we check every bit and send an appropriate warning All strings were checked not to exceed the maximum length of 50 characters.
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Beat Küng authored
estimator status init is not required.
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