Motors update
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@ -25,18 +25,20 @@
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extern const AP_HAL::HAL& hal;
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AP_Motors6DOF::add_motor_raw(int8_t motor_num, float roll_fac, float pitch_fac, float yaw_fac, float throttle_fac, float forward_fac, float strafe_fac, uint8_t testing_order) {
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//Parent takes care of enabling output and setting up masks
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AP_MotorsMatrix::add_motor_raw(motor_num, roll_fac, pitch_fac, yaw_fac, testing_order);
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//void AP_Motors6DOF::add_motor_raw(int8_t motor_num, float roll_fac, float pitch_fac, float yaw_fac, float throttle_fac, float forward_fac, float strafe_fac, uint8_t testing_order) {
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// //Parent takes care of enabling output and setting up masks
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// AP_MotorsMatrix::add_motor_raw(motor_num, roll_fac, pitch_fac, yaw_fac, testing_order);
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//
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// //These are additional parameters for an ROV
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// _throttle_factor[motor_num] = throttle_fac;
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// _forward_factor[motor_num] = forward_fac;
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// _strafe_factor[motor_num] = strafe_fac;
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//}
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//These are additional parameters for an ROV
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_throttle_factor[motor_num] = throttle_fac;
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_forward_factor[motor_num] = forward_fac;
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_strafe_factor[motor_num] = strafe_fac;
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}
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// output_min - sends minimum values out to the motors
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void AP_MotorsMatrix::output_min()
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void AP_Motors6DOF::output_min()
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{
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int8_t i;
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@ -62,55 +64,7 @@ void AP_MotorsMatrix::output_min()
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//ToDo: call in control_rov, to mix inputs with no stabilization control
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void AP_Motors6DOF::output_armed_not_stabilizing()
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{
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// uint8_t i;
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// int16_t throttle_radio_output; // total throttle pwm value, summed onto throttle channel minimum, typically ~1100-1900
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// int16_t motor_out[AP_MOTORS_MAX_NUM_MOTORS]; // final outputs sent to the motors
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// int16_t out_min_pwm = _throttle_radio_min + _min_throttle; // minimum pwm value we can send to the motors
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// int16_t out_max_pwm = _throttle_radio_max; // maximum pwm value we can send to the motors
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//
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// // initialize limits flags
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// limit.roll_pitch = true;
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// limit.yaw = true;
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// limit.throttle_lower = false;
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// limit.throttle_upper = false;
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//
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// int16_t thr_in_min = rel_pwm_to_thr_range(_spin_when_armed_ramped);
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// if (_throttle_control_input <= thr_in_min) {
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// _throttle_control_input = thr_in_min;
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// limit.throttle_lower = true;
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// }
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//
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// if (_throttle_control_input >= _hover_out) {
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// _throttle_control_input = _hover_out;
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// limit.throttle_upper = true;
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// }
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//
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// throttle_radio_output = calc_throttle_radio_output();
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//
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// // set output throttle
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// for (i=0; i<AP_MOTORS_MAX_NUM_MOTORS; i++) {
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// if (motor_enabled[i]) {
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// motor_out[i] = throttle_radio_output;
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// }
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// }
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//
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// if(throttle_radio_output >= out_min_pwm) {
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// // apply thrust curve and voltage scaling
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// for (i=0; i<AP_MOTORS_MAX_NUM_MOTORS; i++) {
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// if (motor_enabled[i]) {
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// motor_out[i] = apply_thrust_curve_and_volt_scaling(motor_out[i], out_min_pwm, out_max_pwm);
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// }
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// }
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// }
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//
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// // send output to each motor
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// hal.rcout->cork();
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// for( i=0; i<AP_MOTORS_MAX_NUM_MOTORS; i++ ) {
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// if( motor_enabled[i] ) {
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// rc_write(i, motor_out[i]);
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// }
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// }
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// hal.rcout->push();
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output_min(); //cut the motors for now
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}
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// output_armed - sends commands to the motors
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@ -128,12 +82,15 @@ void AP_Motors6DOF::output_armed_stabilizing()
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int16_t strafe_pwm;
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int16_t out_min_pwm = 1100; // minimum pwm value we can send to the motors
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int16_t out_max_pwm = 1900; // maximum pwm value we can send to the motors
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int16_t out_mid_pwm = 1500; // mid pwm value we can send to the motors
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// int16_t out_mid_pwm = 1500; // mid pwm value we can send to the motors
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// the is the best throttle we can come up which provides good control without climbing
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float rpy_scale = 1.0; // this is used to scale the roll, pitch and yaw to fit within the motor limits
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// float rpy_scale = 1.0; // this is used to scale the roll, pitch and yaw to fit within the motor limits
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int16_t rpy_out[AP_MOTORS_MAX_NUM_MOTORS]; // buffer so we don't have to multiply coefficients multiple times.
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int16_t linear_out[AP_MOTORS_MAX_NUM_MOTORS]; // 3 linear DOF mix for each motor
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int16_t motor_out[AP_MOTORS_MAX_NUM_MOTORS]; // final outputs sent to the motors
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int16_t rpy_low = 0; // lowest motor value
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@ -22,20 +22,16 @@ public:
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AP_MotorsMatrix(loop_rate, speed_hz)
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{};
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void set_forward(float forward_in) { _forward_in = constrain_float(2*(forward_in-1500),-1000.0f,1000.0f); }; // range 0 ~ 1000
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void set_strafe(float strafe_in) { _strafe_in = constrain_float(2*(strafe_in-1500),-1000.0f,1000.0f); }; // range 0 ~ 1000
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float get_forward() const { return _forward_in; } // range 1100~1900 this is raw pwm value from rc
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float get_strafe() const { return _strafe_in; } // range 1100~1900 this is raw pwm value from rc
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void output_min() override;
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protected:
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//Override MotorsMatrix method
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void add_motor_raw(int8_t motor_num, float roll_fac, float pitch_fac, float yaw_fac, float climb_fac, float forward_fac, float strafe_fac, uint8_t testing_order)
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//void add_motor_raw(int8_t motor_num, float roll_fac, float pitch_fac, float yaw_fac, float climb_fac, float forward_fac, float strafe_fac, uint8_t testing_order);
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void output_armed_not_stabilizing() override;
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void output_armed_stabilizing() override;
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float _forward_in; // last forward input from set_forward caller, raw pwm
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float _strafe_in; // last strafe input from set_strafe caller, raw pwm
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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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@ -65,6 +65,8 @@ public:
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void set_pitch(int16_t pitch_in) { _pitch_control_input = pitch_in; }; // range -4500 ~ 4500
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void set_yaw(int16_t yaw_in) { _yaw_control_input = yaw_in; }; // range -4500 ~ 4500
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void set_throttle(float throttle_in) { _throttle_in = constrain_float(throttle_in,-100.0f,1100.0f); }; // range 0 ~ 1000
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void set_forward(float forward_in) { _strafe_in = constrain_float(forward_in,-100.0f,1100.0f); }; // range 0 ~ 1000
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void set_strafe(float strafe_in) { _strafe_in = constrain_float(strafe_in,-100.0f,1100.0f); }; // range 0 ~ 1000
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void set_stabilizing(bool stabilizing) { _flags.stabilizing = stabilizing; }
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// accessors for roll, pitch, yaw and throttle inputs to motors
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@ -72,6 +74,8 @@ public:
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float get_pitch() const { return _pitch_control_input; }
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float get_yaw() const { return _yaw_control_input; }
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float get_throttle() const { return _throttle_control_input; }
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float get_forward() const { return _forward_control_input; }
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float get_strafe() const { return _strafe_control_input; }
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void set_throttle_filter_cutoff(float filt_hz) { _throttle_filter.set_cutoff_frequency(filt_hz); }
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@ -151,6 +155,8 @@ protected:
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float _roll_control_input; // desired roll control from attitude controllers, +/- 4500
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float _pitch_control_input; // desired pitch control from attitude controller, +/- 4500
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float _throttle_control_input; // desired throttle (thrust) control from attitude controller, 0-1000
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float _forward_control_input; // desired throttle (forward) control from attitude controller, 0-1000
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float _strafe_control_input; // desired throttle (strafe) control from attitude controller, 0-1000
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float _yaw_control_input; // desired yaw control from attitude controller, +/- 4500
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float _throttle_pwm_scalar; // scalar used to convert throttle channel pwm range into 0-1000 range, ~0.8 - 1.0
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float _rpy_pwm_scalar; // scaler used to convert roll, pitch, yaw inputs to pwm range
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@ -159,6 +165,8 @@ protected:
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int16_t _throttle_radio_min; // minimum radio channel pwm
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int16_t _throttle_radio_max; // maximum radio channel pwm
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float _throttle_in; // last throttle input from set_throttle caller
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float _forward_in; // last forward input from set_forward caller
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float _strafe_in; // last strafe input from set_strafe caller
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LowPassFilterFloat _throttle_filter; // throttle input filter
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// battery voltage, current and air pressure compensation variables
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