AP_MotorsMatrix: implement output_to_motors
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cdec8f3387
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@ -98,6 +98,51 @@ void AP_MotorsMatrix::output_min()
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hal.rcout->push();
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}
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void AP_MotorsMatrix::output_to_motors()
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{
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int8_t i;
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int16_t motor_out[AP_MOTORS_MAX_NUM_MOTORS]; // final pwm values sent to the motor
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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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// set motor output based on thrust requests
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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_min;
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}
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}
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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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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] = constrain_int16(_throttle_radio_min + _throttle_low_end_pct * _min_throttle, _throttle_radio_min, _throttle_radio_min + _min_throttle);
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}
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}
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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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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] = calc_thrust_to_pwm(_thrust_rpyt_out[i]);
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}
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}
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break;
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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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}
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// get_motor_mask - returns a bitmask of which outputs are being used for motors (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_MotorsMatrix::get_motor_mask()
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@ -42,6 +42,9 @@ 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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// add_motor using just position and yaw_factor (or prop direction)
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void add_motor(int8_t motor_num, float angle_degrees, float yaw_factor, uint8_t testing_order);
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