We’re debugging AUTO takeoff behavior on a separate fixed-wing flying-wing test platform and are seeing an issue where PX4 never commands a rotation.
In AUTO mode with a standard TAKEOFF mission item:
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The aircraft reaches the takeoff point correctly
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Throttle commands behave as expected
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Elevons remain neutral
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No pitch-up or rotation command is ever generated
Manual and stabilized modes work normally, so control surfaces, mixing, and authority are confirmed to be correct.
We’ve tried adjusting RWTO_TKOFF, TKOFF_THR, and related parameters without any change in behavior, and the mission item appears to be set up correctly.
Relevant details:
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Flying wing (no dedicated elevator, only elevons)
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No airspeed sensor installed
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Bench and ground tests performed with lowered takeoff speeds
What we’re unclear on is:
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What exact conditions PX4 requires before commanding rotation during AUTO takeoff
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Whether the lack of an airspeed sensor can suppress the pitch-up command
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Whether flying wings are handled differently from conventional fixed-wing aircraft
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Whether rotation commands should be observable during bench or low-speed testing, or if PX4 suppresses them until specific airspeed/attitude conditions are met
Documentation on the rotation logic and prerequisites for AUTO takeoff is fairly vague, so any insight into expected behavior here would be appreciated.