mirror of https://github.com/ArduPilot/ardupilot
ACM : revert back to the 2.6 climb rate calc
The current filter is outputting wild oscillations.
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@ -2134,9 +2134,9 @@ static void update_trig(void){
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static void update_altitude()
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static void update_altitude()
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{
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{
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static int16_t old_sonar_alt = 0;
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static int16_t old_sonar_alt = 0;
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static int32_t old_baro_alt = 0;
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#if HIL_MODE == HIL_MODE_ATTITUDE
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#if HIL_MODE == HIL_MODE_ATTITUDE
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static int32_t old_baro_alt = 0;
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// we are in the SIM, fake out the baro and Sonar
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// we are in the SIM, fake out the baro and Sonar
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int16_t fake_relative_alt = g_gps->altitude - gps_base_alt;
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int16_t fake_relative_alt = g_gps->altitude - gps_base_alt;
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baro_alt = fake_relative_alt;
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baro_alt = fake_relative_alt;
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@ -2156,18 +2156,19 @@ static void update_altitude()
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baro_alt = read_barometer();
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baro_alt = read_barometer();
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// calc the vertical accel rate
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// calc the vertical accel rate
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/*
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* // 2.6 way
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// 2.6 way
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* int16_t temp = (baro_alt - old_baro_alt) * 10;
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int16_t temp = (baro_alt - old_baro_alt) * 10;
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* baro_rate = (temp + baro_rate) >> 1;
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baro_rate = (temp + baro_rate) >> 1;
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* baro_rate = constrain(baro_rate, -300, 300);
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baro_rate = constrain(baro_rate, -300, 300);
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* old_baro_alt = baro_alt;
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old_baro_alt = baro_alt;
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*/
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// Using Tridge's new clamb rate calc
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// Using Tridge's new clamb rate calc
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/*
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int16_t temp = barometer.get_climb_rate() * 100;
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int16_t temp = barometer.get_climb_rate() * 100;
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baro_rate = (temp + baro_rate) >> 1;
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baro_rate = (temp + baro_rate) >> 1;
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baro_rate = constrain(baro_rate, -300, 300);
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baro_rate = constrain(baro_rate, -300, 300);
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*/
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#endif
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#endif
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// Note: sonar_alt is calculated in a faster loop and filtered with a mode filter
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// Note: sonar_alt is calculated in a faster loop and filtered with a mode filter
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