mirror of https://github.com/ArduPilot/ardupilot
AP_Motors: removed unused pwm parameters for heli
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@ -123,28 +123,6 @@ const AP_Param::GroupInfo AP_MotorsHeli_Dual::var_info[] = {
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// @Increment: 0.1
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AP_GROUPINFO("YAW_SCALER", 12, AP_MotorsHeli_Dual, _yaw_scaler, 1.0f),
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// @Param: RSC_PWM_MIN
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// @DisplayName: RSC PWM output miniumum
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// @Description: This sets the PWM output on RSC channel for maximum rotor speed
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// @Range: 0 2000
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// @User: Standard
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AP_GROUPINFO("RSC_PWM_MIN", 13, AP_MotorsHeli_Dual, _rotor._pwm_min, 1000),
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// @Param: RSC_PWM_MAX
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// @DisplayName: RSC PWM output maxiumum
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// @Description: This sets the PWM output on RSC channel for miniumum rotor speed
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// @Range: 0 2000
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// @User: Standard
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AP_GROUPINFO("RSC_PWM_MAX", 14, AP_MotorsHeli_Dual, _rotor._pwm_max, 2000),
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// @Param: RSC_PWM_REV
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// @DisplayName: RSC PWM reversal
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// @Description: This controls reversal of the RSC channel output
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// @Values: -1:Reversed,1:Normal
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// @User: Standard
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AP_GROUPINFO("RSC_PWM_REV", 15, AP_MotorsHeli_Dual, _rotor._pwm_rev, 1),
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// @Param: COL2_MIN
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// @DisplayName: Collective Pitch Minimum for rear swashplate
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// @Description: Lowest possible servo position in PWM microseconds for the rear swashplate
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@ -23,27 +23,6 @@ extern const AP_HAL::HAL& hal;
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const AP_Param::GroupInfo AP_MotorsHeli_Quad::var_info[] = {
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AP_NESTEDGROUPINFO(AP_MotorsHeli, 0),
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// @Param: RSC_PWM_MIN
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// @DisplayName: RSC PWM output miniumum
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// @Description: This sets the PWM output on RSC channel for maximum rotor speed
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// @Range: 0 2000
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// @User: Standard
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AP_GROUPINFO("RSC_PWM_MIN", 1, AP_MotorsHeli_Quad, _rotor._pwm_min, 1000),
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// @Param: RSC_PWM_MAX
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// @DisplayName: RSC PWM output maxiumum
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// @Description: This sets the PWM output on RSC channel for miniumum rotor speed
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// @Range: 0 2000
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// @User: Standard
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AP_GROUPINFO("RSC_PWM_MAX", 2, AP_MotorsHeli_Quad, _rotor._pwm_max, 2000),
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// @Param: RSC_PWM_REV
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// @DisplayName: RSC PWM reversal
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// @Description: This controls reversal of the RSC channel output
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// @Values: -1:Reversed,1:Normal
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// @User: Standard
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AP_GROUPINFO("RSC_PWM_REV", 3, AP_MotorsHeli_Quad, _rotor._pwm_rev, 1),
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AP_GROUPEND
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};
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@ -103,10 +103,6 @@ private:
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uint16_t _power_slewrate = 0; // slewrate for throttle (percentage per second)
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float _load_feedforward = 0.0f; // estimate of motor load, range 0-1.0f
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AP_Int16 _pwm_min;
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AP_Int16 _pwm_max;
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AP_Int8 _pwm_rev;
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// update_rotor_ramp - slews rotor output scalar between 0 and 1, outputs float scalar to _rotor_ramp_output
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void update_rotor_ramp(float rotor_ramp_input, float dt);
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