AC_AttitudeControl: rename get_boosted_throttle to get_throttle_boosted
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@ -264,7 +264,7 @@ protected:
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virtual float rate_bf_to_motor_yaw(float rate_target_rads);
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// Compute a throttle value that is adjusted for the tilt angle of the vehicle
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virtual float get_boosted_throttle(float throttle_in) = 0;
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virtual float get_throttle_boosted(float throttle_in) = 0;
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// Return angle in radians to be added to roll angle. Used by heli to counteract
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// tail rotor thrust in hover. Overloaded by AC_Attitude_Heli to return angle.
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@ -125,9 +125,6 @@ private:
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//
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// throttle methods
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//
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// calculate total body frame throttle required to produce the given earth frame throttle
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float get_boosted_throttle(float throttle_in);
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// pass through for roll and pitch
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int16_t _passthrough_roll;
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@ -153,7 +153,7 @@ void AC_AttitudeControl_Multi::set_throttle_out(float throttle_in, bool apply_an
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_throttle_in_filt.apply(throttle_in, _dt);
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_motors.set_throttle_filter_cutoff(filter_cutoff);
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if (apply_angle_boost) {
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_motors.set_throttle(get_boosted_throttle(throttle_in));
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_motors.set_throttle(get_throttle_boosted(throttle_in));
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}else{
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_motors.set_throttle(throttle_in);
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// Clear angle_boost for logging purposes
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@ -163,7 +163,7 @@ void AC_AttitudeControl_Multi::set_throttle_out(float throttle_in, bool apply_an
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// returns a throttle including compensation for roll/pitch angle
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// throttle value should be 0 ~ 1
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float AC_AttitudeControl_Multi::get_boosted_throttle(float throttle_in)
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float AC_AttitudeControl_Multi::get_throttle_boosted(float throttle_in)
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{
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if (!_angle_boost_enabled) {
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_angle_boost = 0;
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@ -59,7 +59,7 @@ public:
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void set_throttle_out(float throttle_in, bool apply_angle_boost, float filt_cutoff) override;
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// calculate total body frame throttle required to produce the given earth frame throttle
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float get_boosted_throttle(float throttle_in);
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float get_throttle_boosted(float throttle_in);
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// user settable parameters
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static const struct AP_Param::GroupInfo var_info[];
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