mirror of https://github.com/ArduPilot/ardupilot
AP_MotorsCoax: output_to_motors implements spool logic
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@ -130,6 +130,47 @@ void AP_MotorsCoax::output_min()
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hal.rcout->push();
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}
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void AP_MotorsCoax::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, calc_pivot_radio_output(_roll_radio_passthrough*_servo_1_reverse, _servo_1_min, _servo_1_trim, _servo_1_max));
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rc_write(AP_MOTORS_MOT_2, calc_pivot_radio_output(_pitch_radio_passthrough *_servo_2_reverse, _servo_2_min, _servo_2_trim, _servo_2_max));
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rc_write(AP_MOTORS_MOT_3, calc_pivot_radio_output(_roll_radio_passthrough*_servo_3_reverse, _servo_3_min, _servo_3_trim, _servo_3_max));
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rc_write(AP_MOTORS_MOT_4, calc_pivot_radio_output(_pitch_radio_passthrough*_servo_4_reverse, _servo_4_min, _servo_4_trim, _servo_4_max));
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rc_write(AP_MOTORS_MOT_5, _throttle_radio_min);
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rc_write(AP_MOTORS_MOT_6, _throttle_radio_min);
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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, calc_pivot_radio_output(_throttle_low_end_pct * _actuator_out[0]*_servo_1_reverse, _servo_1_min, _servo_1_trim, _servo_1_max));
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rc_write(AP_MOTORS_MOT_2, calc_pivot_radio_output(_throttle_low_end_pct * _actuator_out[1]*_servo_2_reverse, _servo_2_min, _servo_2_trim, _servo_2_max));
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rc_write(AP_MOTORS_MOT_3, calc_pivot_radio_output(_throttle_low_end_pct * _actuator_out[2]*_servo_3_reverse, _servo_3_min, _servo_3_trim, _servo_3_max));
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rc_write(AP_MOTORS_MOT_4, calc_pivot_radio_output(_throttle_low_end_pct * _actuator_out[3]*_servo_4_reverse, _servo_4_min, _servo_4_trim, _servo_4_max));
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rc_write(AP_MOTORS_MOT_5, 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_6, constrain_int16(_throttle_radio_min + _throttle_low_end_pct * _min_throttle, _throttle_radio_min, _throttle_radio_min + _min_throttle));
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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_pivot_radio_output(_actuator_out[0]*_servo_1_reverse, _servo_1_min, _servo_1_trim, _servo_1_max));
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rc_write(AP_MOTORS_MOT_2, calc_pivot_radio_output(_actuator_out[1]*_servo_2_reverse, _servo_2_min, _servo_2_trim, _servo_2_max));
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rc_write(AP_MOTORS_MOT_3, calc_pivot_radio_output(_actuator_out[2]*_servo_3_reverse, _servo_3_min, _servo_3_trim, _servo_3_max));
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rc_write(AP_MOTORS_MOT_4, calc_pivot_radio_output(_actuator_out[3]*_servo_4_reverse, _servo_4_min, _servo_4_trim, _servo_4_max));
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rc_write(AP_MOTORS_MOT_5, calc_thrust_to_pwm(_thrust_yt_ccw));
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rc_write(AP_MOTORS_MOT_6, calc_thrust_to_pwm(_thrust_yt_cw));
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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_MotorsCoax::get_motor_mask()
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@ -52,6 +52,9 @@ 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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