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https://github.com/ArduPilot/ardupilot
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AP_Motors: Add current limiting to 6DOF motors for Sub
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@ -17,6 +17,7 @@
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* AP_Motors6DOF.cpp - ArduSub motors library
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*/
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#include <AP_BattMonitor/AP_BattMonitor.h>
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#include <AP_HAL/AP_HAL.h>
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#include "AP_Motors6DOF.h"
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@ -266,6 +267,11 @@ void AP_Motors6DOF::output_to_motors()
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}
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}
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float AP_Motors6DOF::get_current_limit_max_throttle()
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{
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return 1.0f;
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}
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// output_armed - sends commands to the motors
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// includes new scaling stability patch
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// TODO pull code that is common to output_armed_not_stabilizing into helper functions
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@ -338,6 +344,43 @@ void AP_Motors6DOF::output_armed_stabilizing()
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}
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}
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}
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const AP_BattMonitor &battery = AP::battery();
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// Current limiting
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if (_batt_current_max <= 0.0f || !battery.has_current()) {
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return;
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}
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float _batt_current = battery.current_amps();
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float _batt_current_delta = _batt_current - _batt_current_last;
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float loop_interval = 1.0f/_loop_rate;
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float _current_change_rate = _batt_current_delta / loop_interval;
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float predicted_current = _batt_current + (_current_change_rate * loop_interval * 5);
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float batt_current_ratio = _batt_current/_batt_current_max;
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float predicted_current_ratio = predicted_current/_batt_current_max;
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_batt_current_last = _batt_current;
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if (predicted_current > _batt_current_max * 1.5f) {
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batt_current_ratio = 2.5f;
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} else if (_batt_current < _batt_current_max && predicted_current > _batt_current_max) {
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batt_current_ratio = predicted_current_ratio;
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}
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_output_limited += (loop_interval/(loop_interval+_batt_current_time_constant)) * (1 - batt_current_ratio);
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_output_limited = constrain_float(_output_limited, 0.0f, 1.0f);
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for (uint8_t i = 0; i < AP_MOTORS_MAX_NUM_MOTORS; i++) {
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if (motor_enabled[i]) {
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_thrust_rpyt_out[i] *= _output_limited;
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}
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}
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}
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// output_armed - sends commands to the motors
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@ -45,6 +45,8 @@ public:
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static const struct AP_Param::GroupInfo var_info[];
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protected:
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// return current_limit as a number from 0 ~ 1 in the range throttle_min to throttle_max
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float get_current_limit_max_throttle() override;
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//Override MotorsMatrix method
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void add_motor_raw_6dof(int8_t motor_num, float roll_fac, float pitch_fac, float yaw_fac, float climb_fac, float forward_fac, float lat_fac, uint8_t testing_order);
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@ -60,4 +62,8 @@ protected:
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float _throttle_factor[AP_MOTORS_MAX_NUM_MOTORS]; // each motors contribution to throttle (climb/descent)
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float _forward_factor[AP_MOTORS_MAX_NUM_MOTORS]; // each motors contribution to forward/backward
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float _lateral_factor[AP_MOTORS_MAX_NUM_MOTORS]; // each motors contribution to lateral (left/right)
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// current limiting
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float _output_limited = 1.0f;
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float _batt_current_last = 0.0f;
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};
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@ -111,7 +111,7 @@ protected:
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virtual void update_throttle_filter();
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// return current_limit as a number from 0 ~ 1 in the range throttle_min to throttle_max
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float get_current_limit_max_throttle();
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virtual float get_current_limit_max_throttle();
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// apply_thrust_curve_and_volt_scaling - returns throttle in the range 0 ~ 1
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float apply_thrust_curve_and_volt_scaling(float thrust) const;
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