mirror of https://github.com/ArduPilot/ardupilot
AP_MotorsTri: implement output_to_motors for spool logic
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@ -122,6 +122,41 @@ void AP_MotorsTri::output_min()
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hal.rcout->push();
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}
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void AP_MotorsTri::output_to_motors()
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{
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switch (_multicopter_flags.spool_mode) {
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case SHUT_DOWN:
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// sends minimum values out to the motors
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hal.rcout->cork();
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rc_write(AP_MOTORS_MOT_1, _throttle_radio_min);
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rc_write(AP_MOTORS_MOT_2, _throttle_radio_min);
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rc_write(AP_MOTORS_MOT_4, _throttle_radio_min);
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rc_write(AP_MOTORS_CH_TRI_YAW, _yaw_servo_trim);
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hal.rcout->push();
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break;
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case SPIN_WHEN_ARMED:
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// sends output to motors when armed but not flying
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hal.rcout->cork();
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rc_write(AP_MOTORS_MOT_1, constrain_int16(_throttle_radio_min + _throttle_low_end_pct * _min_throttle, _throttle_radio_min, _throttle_radio_min + _min_throttle));
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rc_write(AP_MOTORS_MOT_2, constrain_int16(_throttle_radio_min + _throttle_low_end_pct * _min_throttle, _throttle_radio_min, _throttle_radio_min + _min_throttle));
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rc_write(AP_MOTORS_MOT_4, constrain_int16(_throttle_radio_min + _throttle_low_end_pct * _min_throttle, _throttle_radio_min, _throttle_radio_min + _min_throttle));
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rc_write(AP_MOTORS_CH_TRI_YAW, _yaw_servo_trim);
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hal.rcout->push();
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break;
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case SPOOL_UP:
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case THROTTLE_UNLIMITED:
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case SPOOL_DOWN:
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// set motor output based on thrust requests
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hal.rcout->cork();
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rc_write(AP_MOTORS_MOT_1, calc_thrust_to_pwm(_thrust_right));
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rc_write(AP_MOTORS_MOT_2, calc_thrust_to_pwm(_thrust_left));
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rc_write(AP_MOTORS_MOT_4, calc_thrust_to_pwm(_thrust_rear));
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rc_write(AP_MOTORS_CH_TRI_YAW, calc_yaw_radio_output(_pivot_angle, _pivot_angle_max));
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hal.rcout->push();
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break;
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}
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}
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// get_motor_mask - returns a bitmask of which outputs are being used for motors or servos (1 means being used)
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// this can be used to ensure other pwm outputs (i.e. for servos) do not conflict
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uint16_t AP_MotorsTri::get_motor_mask()
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@ -305,22 +340,13 @@ void AP_MotorsTri::output_test(uint8_t motor_seq, int16_t pwm)
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}
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// calc_yaw_radio_output - calculate final radio output for yaw channel
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int16_t AP_MotorsTri::calc_yaw_radio_output()
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int16_t AP_MotorsTri::calc_yaw_radio_output(float yaw_input, float yaw_input_max)
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{
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int16_t ret;
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if (_yaw_servo_reverse < 0) {
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if (_yaw_control_input >= 0){
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ret = (_yaw_servo_trim - (_yaw_control_input/4500 * (_yaw_servo_trim - _yaw_servo_min)));
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} else {
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ret = (_yaw_servo_trim - (_yaw_control_input/4500 * (_yaw_servo_max - _yaw_servo_trim)));
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}
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if (yaw_input >= 0){
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ret = (_yaw_servo_trim + (yaw_input/yaw_input_max * (_yaw_servo_max - _yaw_servo_trim)));
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} else {
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if (_yaw_control_input >= 0){
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ret = ((_yaw_control_input/4500 * (_yaw_servo_max - _yaw_servo_trim)) + _yaw_servo_trim);
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} else {
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ret = ((_yaw_control_input/4500 * (_yaw_servo_trim - _yaw_servo_min)) + _yaw_servo_trim);
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}
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ret = (_yaw_servo_trim + (yaw_input/yaw_input_max * (_yaw_servo_trim - _yaw_servo_min)));
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}
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return ret;
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@ -40,6 +40,9 @@ public:
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// output_min - sends minimum values out to the motors
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virtual void output_min();
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// output_to_motors - sends minimum values out to the motors
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virtual void output_to_motors();
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// get_motor_mask - returns a bitmask of which outputs are being used for motors or servos (1 means being used)
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// this can be used to ensure other pwm outputs (i.e. for servos) do not conflict
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virtual uint16_t get_motor_mask();
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