mirror of https://github.com/ArduPilot/ardupilot
Copter: add motor thrust lost check
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@ -700,6 +700,7 @@ private:
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// crash_check.cpp
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void crash_check();
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void thrust_loss_check();
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void parachute_check();
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void parachute_release();
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void parachute_manual_release();
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@ -5,6 +5,11 @@
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#define CRASH_CHECK_ANGLE_DEVIATION_DEG 30.0f // 30 degrees beyond angle max is signal we are inverted
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#define CRASH_CHECK_ACCEL_MAX 3.0f // vehicle must be accelerating less than 3m/s/s to be considered crashed
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// Code to detect a thrust loss main ArduCopter code
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#define THRUST_LOSS_CHECK_TRIGGER_SEC 1 // 1 second decent while level and high throttle indictes thrust loss
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#define THRUST_LOSS_CHECK_ANGLE_DEVIATION_CD 150 // we can't expect to maintain altitude beyond 15 degrees on all aircraft
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#define THRUST_LOSS_CHECK_MINIMUM_THROTTLE 0.9f // we can expect to maintain altitude above 90 % throttle
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// crash_check - disarms motors if a crash has been detected
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// crashes are detected by the vehicle being more than 20 degrees beyond it's angle limits continuously for more than 1 second
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// called at MAIN_LOOP_RATE
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@ -53,6 +58,65 @@ void Copter::crash_check()
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}
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}
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// crash_check - disarms motors if a crash has been detected
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// crashes are detected by the vehicle being more than 20 degrees beyond it's angle limits continuously for more than 1 second
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// called at MAIN_LOOP_RATE
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void Copter::thrust_loss_check()
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{
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static uint16_t thrust_loss_counter; // number of iterations vehicle may have been crashed
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// exit immediately if motor failure handling already engaged
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if (motors->get_thrust_boost()) {
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return;
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}
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// return immediately if disarmed
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if (!motors->armed() || ap.land_complete) {
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thrust_loss_counter = 0;
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return;
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}
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// check for desired angle over 15 degrees
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// todo: add thrust angle to AC_AttitudeControl
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const Vector3f angle_target = attitude_control->get_att_target_euler_cd();
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if ((fabs(angle_target.x) > THRUST_LOSS_CHECK_ANGLE_DEVIATION_CD) || (fabs(angle_target.y) > THRUST_LOSS_CHECK_ANGLE_DEVIATION_CD)) {
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thrust_loss_counter = 0;
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return;
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}
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// check for throttle over 90 % or throttle saturation
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if ((attitude_control->get_throttle_in() < THRUST_LOSS_CHECK_MINIMUM_THROTTLE) && (!motors->limit.throttle_upper)) {
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thrust_loss_counter = 0;
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return;
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}
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// check for throttle over 90 % or throttle saturation
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if ((attitude_control->get_throttle_in() < 0.25f)) {
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thrust_loss_counter = 0;
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return;
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}
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// check for decent
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if (inertial_nav.get_velocity_z() >= 0.0f) {
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thrust_loss_counter = 0;
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return;
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}
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// we may be crashing
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thrust_loss_counter++;
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// check if thrust loss for 1 second
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if (thrust_loss_counter >= (THRUST_LOSS_CHECK_TRIGGER_SEC * scheduler.get_loop_rate_hz())) {
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// log an error in the dataflash
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Log_Write_Error(ERROR_SUBSYSTEM_THRUST_LOSS_CHECK, ERROR_CODE_FAILSAFE_OCCURRED);
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// send message to gcs
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//gcs().send_text(MAV_SEVERITY_EMERGENCY,"Potential Thrust Loss");
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gcs().send_text(MAV_SEVERITY_EMERGENCY, "Potential Thrust Loss (%d)", (int)motors->get_lost_motor());
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// enable thrust loss handling
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motors->set_thrust_boost(true);
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}
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}
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#if PARACHUTE == ENABLED
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// Code to detect a crash main ArduCopter code
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@ -360,6 +360,7 @@ enum LoggingParameters {
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#define ERROR_SUBSYSTEM_NAVIGATION 22
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#define ERROR_SUBSYSTEM_FAILSAFE_TERRAIN 23
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#define ERROR_SUBSYSTEM_EKF_PRIMARY 24
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#define ERROR_SUBSYSTEM_THRUST_LOSS_CHECK 25
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// general error codes
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#define ERROR_CODE_ERROR_RESOLVED 0
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#define ERROR_CODE_FAILED_TO_INITIALISE 1
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@ -26,6 +26,7 @@ void Copter::update_land_and_crash_detectors()
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#endif
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crash_check();
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thrust_loss_check();
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}
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// update_land_detector - checks if we have landed and updates the ap.land_complete flag
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