mirror of https://github.com/ArduPilot/ardupilot
AC_AutoTune: fix pilot testing bug
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5eede68dce
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@ -198,29 +198,32 @@ void AC_AutoTune::run()
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const bool zero_rp_input = is_zero(target_roll_cd) && is_zero(target_pitch_cd);
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const uint32_t now = AP_HAL::millis();
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if (!zero_rp_input || !is_zero(target_yaw_rate_cds) || !is_zero(target_climb_rate_cms)) {
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if (!pilot_override) {
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pilot_override = true;
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// set gains to their original values
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load_gains(GAIN_ORIGINAL);
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attitude_control->use_sqrt_controller(true);
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}
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// reset pilot override time
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override_time = now;
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if (!zero_rp_input) {
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// only reset position on roll or pitch input
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have_position = false;
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}
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} else if (pilot_override) {
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// check if we should resume tuning after pilot's override
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if (now - override_time > AUTOTUNE_PILOT_OVERRIDE_TIMEOUT_MS) {
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pilot_override = false; // turn off pilot override
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// set gains to their intra-test values (which are very close to the original gains)
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// load_gains(GAIN_INTRA_TEST); //I think we should be keeping the originals here to let the I term settle quickly
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step = WAITING_FOR_LEVEL; // set tuning step back from beginning
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step_start_time_ms = now;
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level_start_time_ms = now;
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desired_yaw_cd = ahrs_view->yaw_sensor;
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if (mode != SUCCESS) {
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if (!zero_rp_input || !is_zero(target_yaw_rate_cds) || !is_zero(target_climb_rate_cms)) {
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if (!pilot_override) {
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pilot_override = true;
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// set gains to their original values
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load_gains(GAIN_ORIGINAL);
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attitude_control->use_sqrt_controller(true);
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}
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// reset pilot override time
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override_time = now;
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if (!zero_rp_input) {
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// only reset position on roll or pitch input
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have_position = false;
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}
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} else if (pilot_override) {
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// check if we should resume tuning after pilot's override
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if (now - override_time > AUTOTUNE_PILOT_OVERRIDE_TIMEOUT_MS) {
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pilot_override = false; // turn off pilot override
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// set gains to their intra-test values (which are very close to the original gains)
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// load_gains(GAIN_INTRA_TEST); //I think we should be keeping the originals here to let the I term settle quickly
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step = WAITING_FOR_LEVEL; // set tuning step back from beginning
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step_start_time_ms = now;
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level_start_time_ms = now;
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desired_yaw_cd = ahrs_view->yaw_sensor;
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}
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}
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}
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if (pilot_override) {
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