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https://github.com/ArduPilot/ardupilot
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AP_Motors: refactor apply_thrust_curve_and_volt_scaling
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@ -289,12 +289,19 @@ void AP_Motors::current_limit_max_throttle()
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// apply_thrust_curve_and_volt_scaling - returns throttle curve adjusted pwm value (i.e. 1000 ~ 2000)
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int16_t AP_Motors::apply_thrust_curve_and_volt_scaling(int16_t pwm_out, int16_t pwm_min, int16_t pwm_max) const
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{
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float temp_out = ((float)(pwm_out-pwm_min))/((float)(pwm_max-pwm_min));
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// convert to 0.0 to 1.0 ratio
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float throttle_ratio = ((float)(pwm_out-pwm_min))/((float)(pwm_max-pwm_min));
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// apply thrust curve - domain 0.0 to 1.0, range 0.0 to 1.0
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if (_thrust_curve_expo > 0.0f){
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temp_out = ((_thrust_curve_expo-1.0f) + safe_sqrt((1.0f-_thrust_curve_expo)*(1.0f-_thrust_curve_expo) + 4.0f*_thrust_curve_expo*_lift_max*temp_out))/(2.0f*_thrust_curve_expo*_batt_voltage_filt.get());
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throttle_ratio = ((_thrust_curve_expo-1.0f) + safe_sqrt((1.0f-_thrust_curve_expo)*(1.0f-_thrust_curve_expo) + 4.0f*_thrust_curve_expo*_lift_max*throttle_ratio))/(2.0f*_thrust_curve_expo*_batt_voltage_filt.get());
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}
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temp_out = constrain_float(temp_out*_thrust_curve_max*(pwm_max-pwm_min)+pwm_min, pwm_min, pwm_max);
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return (int16_t)temp_out;
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// scale to maximum thrust point
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throttle_ratio *= _thrust_curve_max;
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// convert back to pwm range, constrain and return
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return (int16_t)constrain_float(throttle_ratio*(pwm_max-pwm_min)+pwm_min, pwm_min, (pwm_max-pwm_min)*_thrust_curve_max+pwm_min);
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}
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// update_lift_max from battery voltage - used for voltage compensation
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