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@ -7,8 +7,8 @@
@@ -7,8 +7,8 @@
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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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#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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@ -58,9 +58,7 @@ void Copter::crash_check()
@@ -58,9 +58,7 @@ 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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// check for loss of thrust and trigger thrust boost in motors library
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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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@ -79,18 +77,18 @@ void Copter::thrust_loss_check()
@@ -79,18 +77,18 @@ void Copter::thrust_loss_check()
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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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if ((fabsf(angle_target.x) > THRUST_LOSS_CHECK_ANGLE_DEVIATION_CD) || (fabsf(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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// 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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// check throttle is over 25%
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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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@ -102,7 +100,7 @@ void Copter::thrust_loss_check()
@@ -102,7 +100,7 @@ void Copter::thrust_loss_check()
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return; |
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} |
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// we may be crashing
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// we may have lost thrust
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thrust_loss_counter++; |
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// check if thrust loss for 1 second
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@ -110,8 +108,7 @@ void Copter::thrust_loss_check()
@@ -110,8 +108,7 @@ void Copter::thrust_loss_check()
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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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gcs_send_text_fmt(MAV_SEVERITY_EMERGENCY, "Potential Thrust Loss (%d)", (int)motors->get_lost_motor() + 1); |
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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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