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@ -861,7 +861,7 @@ void AP_TECS::_update_pitch(void)
@@ -861,7 +861,7 @@ void AP_TECS::_update_pitch(void)
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// integrator has to catch up before the nose can be raised to reduce speed during climbout.
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// During flare a different damping gain is used
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float gainInv = (_TAS_state * timeConstant() * GRAVITY_MSS); |
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float temp = SEB_error + SEBdot_dem * timeConstant(); |
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float temp = SEB_error + 0.5*SEBdot_dem * timeConstant(); |
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float pitch_damp = _ptchDamp; |
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if (_landing.is_flaring()) { |
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