mirror of https://github.com/ArduPilot/ardupilot
Copter: compassmot format fixes
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@ -29,7 +29,7 @@ MAV_RESULT Copter::mavlink_compassmot(mavlink_channel_t chan)
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if (ap.compass_mot) {
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// ignore restart messages
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return MAV_RESULT_TEMPORARILY_REJECTED;
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}else{
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} else {
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ap.compass_mot = true;
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}
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@ -88,7 +88,7 @@ MAV_RESULT Copter::mavlink_compassmot(mavlink_channel_t chan)
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// default compensation type to use current if possible
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if (battery.has_current()) {
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comp_type = AP_COMPASS_MOT_COMP_CURRENT;
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}else{
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} else {
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comp_type = AP_COMPASS_MOT_COMP_THROTTLE;
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}
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@ -104,7 +104,7 @@ MAV_RESULT Copter::mavlink_compassmot(mavlink_channel_t chan)
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// inform what type of compensation we are attempting
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if (comp_type == AP_COMPASS_MOT_COMP_CURRENT) {
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gcs_chan.send_text(MAV_SEVERITY_INFO, "Current");
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} else{
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} else {
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gcs_chan.send_text(MAV_SEVERITY_INFO, "Throttle");
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}
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@ -153,18 +153,18 @@ MAV_RESULT Copter::mavlink_compassmot(mavlink_channel_t chan)
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// read radio input
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read_radio();
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// pass through throttle to motors
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SRV_Channels::cork();
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motors->set_throttle_passthrough_for_esc_calibration(channel_throttle->get_control_in() / 1000.0f);
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SRV_Channels::push();
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// read some compass values
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compass.read();
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// read current
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battery.read();
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// calculate scaling for throttle
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throttle_pct = (float)channel_throttle->get_control_in() / 1000.0f;
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throttle_pct = constrain_float(throttle_pct,0.0f,1.0f);
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@ -174,8 +174,6 @@ MAV_RESULT Copter::mavlink_compassmot(mavlink_channel_t chan)
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for (uint8_t i=0; i<compass.get_count(); i++) {
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compass_base[i] = compass_base[i] * 0.99f + compass.get_field(i) * 0.01f;
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}
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// causing printing to happen as soon as throttle is lifted
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} else {
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// calculate diff from compass base and scale with throttle
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@ -192,14 +190,13 @@ MAV_RESULT Copter::mavlink_compassmot(mavlink_channel_t chan)
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// adjust the motor compensation to negate the impact
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motor_compensation[i] = motor_compensation[i] * 0.99f - motor_impact_scaled[i] * 0.01f;
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}
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updated = true;
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} else {
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// for each compass
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for (uint8_t i=0; i<compass.get_count(); i++) {
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// current based compensation if more than 3amps being drawn
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motor_impact_scaled[i] = motor_impact[i] / battery.current_amps();
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// adjust the motor compensation to negate the impact if drawing over 3amps
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if (battery.current_amps() >= 3.0f) {
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motor_compensation[i] = motor_compensation[i] * 0.99f - motor_impact_scaled[i] * 0.01f;
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@ -214,7 +211,7 @@ MAV_RESULT Copter::mavlink_compassmot(mavlink_channel_t chan)
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// interference is impact@fullthrottle / mag field * 100
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interference_pct[i] = motor_compensation[i].length() / (float)arming.compass_magfield_expected() * 100.0f;
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}
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}else{
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} else {
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for (uint8_t i=0; i<compass.get_count(); i++) {
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// interference is impact/amp * (max current seen / max throttle seen) / mag field * 100
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interference_pct[i] = motor_compensation[i].length() * (current_amps_max/throttle_pct_max) / (float)arming.compass_magfield_expected() * 100.0f;
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@ -224,8 +221,8 @@ MAV_RESULT Copter::mavlink_compassmot(mavlink_channel_t chan)
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// record maximum throttle and current
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throttle_pct_max = MAX(throttle_pct_max, throttle_pct);
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current_amps_max = MAX(current_amps_max, battery.current_amps());
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}
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if (AP_HAL::millis() - last_send_time > 500) {
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last_send_time = AP_HAL::millis();
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mavlink_msg_compassmot_status_send(chan,
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@ -275,4 +272,3 @@ MAV_RESULT Copter::mavlink_compassmot(mavlink_channel_t chan)
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return MAV_RESULT_ACCEPTED;
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#endif // FRAME_CONFIG != HELI_FRAME
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}
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