We’re debugging AUTO takeoff behavior on a fixed-wing flying-wing platform in ArduPilot and are seeing an issue where the aircraft 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 ramps as expected
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Elevons remain neutral
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No pitch-up / rotation command is issued
Manual and assisted fixed-wing modes work normally, so control surfaces, mixing, and authority appear correct.
We’ve been trying to debug this using ground and roll testing (including reduced takeoff speeds to observe behavior safely), but so far we haven’t seen any pitch command generated during AUTO takeoff. Adjusting takeoff-related settings hasn’t changed the behavior.
Relevant details:
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Flying wing (elevons only, no dedicated elevator)
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No airspeed sensor installed
What we’re unclear on:
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What conditions ArduPilot requires before issuing a rotation command during AUTO takeoff
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Whether the lack of an airspeed sensor can suppress pitch-up behavior
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Whether flying wings are treated differently from conventional fixed-wing aircraft during AUTO takeoff
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Whether rotation commands should be observable during roll/bench testing, or if ArduPilot suppresses pitch commands until specific speed or attitude conditions are met
The documentation is vague on the exact gating logic for AUTO takeoff rotation, particularly for flying wings, so any insight into expected behavior or required prerequisites would be very helpful.