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https://github.com/ArduPilot/ardupilot
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TECS: set landing params as private and use accessors
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@ -981,7 +981,7 @@ void AP_TECS::update_pitch_throttle(int32_t hgt_dem_cm,
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if (flight_stage == FLIGHT_LAND_FINAL) {
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// in flare use min pitch from LAND_PITCH_CD
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_PITCHminf = MAX(_PITCHminf, _landing.pitch_cd * 0.01f);
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_PITCHminf = MAX(_PITCHminf, _landing.get_pitch_cd() * 0.01f);
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// and use max pitch from TECS_LAND_PMAX
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if (_land_pitch_max != 0) {
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@ -994,15 +994,15 @@ void AP_TECS::update_pitch_throttle(int32_t hgt_dem_cm,
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// constrain the pitch in landing as we get close to the flare
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// point. Use a simple linear limit from 15 meters after the
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// landing point
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float time_to_flare = (- hgt_afe / _climb_rate) - _landing.flare_sec;
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float time_to_flare = (- hgt_afe / _climb_rate) - _landing.get_flare_sec();
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if (time_to_flare < 0) {
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// we should be flaring already
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_PITCHminf = MAX(_PITCHminf, _landing.pitch_cd * 0.01f);
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_PITCHminf = MAX(_PITCHminf, _landing.get_pitch_cd() * 0.01f);
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} else if (time_to_flare < timeConstant()*2) {
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// smoothly move the min pitch to the flare min pitch over
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// twice the time constant
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float p = time_to_flare/(2*timeConstant());
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float pitch_limit_cd = p*aparm.pitch_limit_min_cd + (1-p)*_landing.pitch_cd;
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float pitch_limit_cd = p*aparm.pitch_limit_min_cd + (1-p)*_landing.get_pitch_cd();
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#if 0
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::printf("ttf=%.1f hgt_afe=%.1f _PITCHminf=%.1f pitch_limit=%.1f climb=%.1f\n",
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time_to_flare, hgt_afe, _PITCHminf, pitch_limit_cd*0.01f, _climb_rate);
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