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SITL: fixed pitch constraint on fixed wing takeoff
fixes issue with jet takeoff
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@ -554,7 +554,14 @@ void Aircraft::update_dynamics(const Vector3f &rot_accel)
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// zero roll/pitch, but keep yaw
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float r, p, y;
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dcm.to_euler(&r, &p, &y);
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dcm.from_euler(0.0f, 0.0f, y);
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if (velocity_ef.length() < 5) {
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// at high speeds don't constrain pitch, otherwise we
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// can get stuck in takeoff
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p = 0;
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} else {
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p = MAX(p, 0);
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}
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dcm.from_euler(0.0f, p, y);
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// only fwd movement
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Vector3f v_bf = dcm.transposed() * velocity_ef;
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v_bf.y = 0.0f;
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