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@ -240,7 +240,7 @@ void AP_MotorsMulticopter::current_limit_max_throttle()
@@ -240,7 +240,7 @@ void AP_MotorsMulticopter::current_limit_max_throttle()
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} |
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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_MotorsMulticopter::apply_thrust_curve_and_volt_scaling(int16_t pwm_out, int16_t pwm_min, int16_t pwm_max) const |
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int16_t AP_MotorsMulticopter::apply_thrust_curve_and_volt_scaling_pwm(int16_t pwm_out, int16_t pwm_min, int16_t pwm_max) const |
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{ |
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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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@ -257,6 +257,21 @@ int16_t AP_MotorsMulticopter::apply_thrust_curve_and_volt_scaling(int16_t pwm_ou
@@ -257,6 +257,21 @@ int16_t AP_MotorsMulticopter::apply_thrust_curve_and_volt_scaling(int16_t pwm_ou
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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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// apply_thrust_curve_and_volt_scaling - returns throttle in the range 0 ~ 1
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float AP_MotorsMulticopter::apply_thrust_curve_and_volt_scaling(float thrust) const |
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{ |
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float throttle_ratio = thrust; |
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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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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*thrust))/(2.0f*_thrust_curve_expo*_batt_voltage_filt.get()); |
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} |
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// scale to maximum thrust point
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throttle_ratio *= _thrust_curve_max; |
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return constrain_float(throttle_ratio, 0.0f, _thrust_curve_max); |
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} |
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// update_lift_max from battery voltage - used for voltage compensation
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void AP_MotorsMulticopter::update_lift_max_from_batt_voltage() |
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{ |
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