Files
PX4-Autopilot/src
Paul Riseborough d783bc8ae1 commander: Check for nav divergence due to bad yaw at takeoff
This check is performed for up to 30 seconds after takeoff or until  a horizontal speed of 5 m/s has been achieved.
If the vehicle is not landed and the check is active, then the yaw will be declared as failed if the velocity innovations fail for a continuous period of 1 second.
This will cause the local and global position and velocity validity to be latched false to prevent unsafe use of position control modes.
2017-12-04 09:09:54 +00:00
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