mirror of https://github.com/ArduPilot/ardupilot
AP_Motors: tailsiter remove push of plane ouputs
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50d95943e3
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@ -81,16 +81,13 @@ void AP_MotorsTailsitter::output_to_motors()
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if (!_flags.initialised_ok) {
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return;
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}
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float throttle_pwm = 0.0f;
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switch (_spool_mode) {
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case SHUT_DOWN:
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throttle_pwm = get_pwm_output_min();
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SRV_Channels::set_output_pwm(SRV_Channel::k_throttleLeft, get_pwm_output_min());
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SRV_Channels::set_output_pwm(SRV_Channel::k_throttleRight, get_pwm_output_min());
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break;
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case GROUND_IDLE:
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throttle_pwm = output_to_pwm(actuator_spin_up_to_ground_idle());
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set_actuator_with_slew(_actuator[1], actuator_spin_up_to_ground_idle());
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SRV_Channels::set_output_pwm(SRV_Channel::k_throttleLeft, output_to_pwm(actuator_spin_up_to_ground_idle()));
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SRV_Channels::set_output_pwm(SRV_Channel::k_throttleRight, output_to_pwm(actuator_spin_up_to_ground_idle()));
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@ -98,7 +95,6 @@ void AP_MotorsTailsitter::output_to_motors()
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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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throttle_pwm = output_to_pwm(thrust_to_actuator(_throttle));
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SRV_Channels::set_output_pwm(SRV_Channel::k_throttleLeft, output_to_pwm(thrust_to_actuator(_thrust_left)));
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SRV_Channels::set_output_pwm(SRV_Channel::k_throttleRight, output_to_pwm(thrust_to_actuator(_thrust_right)));
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break;
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@ -108,11 +104,6 @@ void AP_MotorsTailsitter::output_to_motors()
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SRV_Channels::set_output_scaled(SRV_Channel::k_tiltMotorLeft, _tilt_left*SERVO_OUTPUT_RANGE);
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SRV_Channels::set_output_scaled(SRV_Channel::k_tiltMotorRight, _tilt_right*SERVO_OUTPUT_RANGE);
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// plane outputs for Qmodes are setup here, and written to the HAL by the plane servos loop
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SRV_Channels::set_output_scaled(SRV_Channel::k_aileron, -_yaw_in*SERVO_OUTPUT_RANGE);
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SRV_Channels::set_output_scaled(SRV_Channel::k_elevator, _pitch_in*SERVO_OUTPUT_RANGE);
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SRV_Channels::set_output_scaled(SRV_Channel::k_rudder, _roll_in*SERVO_OUTPUT_RANGE);
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SRV_Channels::set_output_pwm(SRV_Channel::k_throttle, throttle_pwm);
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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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