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AP_TECS: bug fix - use takeoff integrator during land abort

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This commit is contained in:
Tom Pittenger 2017-01-10 21:32:41 -08:00
parent 817efe9b6d
commit d1434602a5
1 changed files with 1 additions and 1 deletions
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2
libraries/AP_TECS/AP_TECS.cpp
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@ -682,7 +682,7 @@ void AP_TECS::_update_throttle_with_airspeed(void)
float AP_TECS::_get_i_gain(void)
{
float i_gain = _integGain;
if (_flight_stage == AP_Vehicle::FixedWing::FLIGHT_TAKEOFF) {
if (_flight_stage == AP_Vehicle::FixedWing::FLIGHT_TAKEOFF || _flight_stage == AP_Vehicle::FixedWing::FLIGHT_ABORT_LAND) {
if (!is_zero(_integGain_takeoff)) {
i_gain = _integGain_takeoff;
}