forked from Archive/PX4-Autopilot
Merge pull request #372 from PX4/pr-tecs_init
TECS initialize throttle integrator at cruise if in air
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bdbc05cf91
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@ -531,7 +531,7 @@ void TECS::_initialize_states(float pitch, float throttle_cruise, float baro_alt
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_vert_pos_state = baro_altitude;
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_tas_rate_state = 0.0f;
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_tas_state = _EAS * EAS2TAS;
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_throttle_integ_state = 0.0f;
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_throttle_integ_state = (_in_air ? throttle_cruise : 0.0f);
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_pitch_integ_state = 0.0f;
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_last_throttle_setpoint = throttle_cruise;
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_last_pitch_setpoint = constrain(pitch, _pitch_setpoint_min, _pitch_setpoint_max);
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