Copter: get_pilot_desired_climb_rate accepts control_in as 0 to 1000
Previously the input was expected to be throttle_min (i.e. 130) to 1000
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@ -161,8 +161,7 @@ float Copter::get_pilot_desired_throttle(int16_t throttle_control)
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return throttle_out;
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}
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// get_pilot_desired_climb_rate - transform pilot's throttle input to
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// climb rate in cm/s. we use radio_in instead of control_in to get the full range
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// get_pilot_desired_climb_rate - transform pilot's throttle input to climb rate in cm/s
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// without any deadzone at the bottom
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float Copter::get_pilot_desired_climb_rate(float throttle_control)
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{
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@ -177,7 +176,7 @@ float Copter::get_pilot_desired_climb_rate(float throttle_control)
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float deadband_bottom = mid_stick - g.throttle_deadzone;
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// ensure a reasonable throttle value
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throttle_control = constrain_float(throttle_control,g.throttle_min,1000.0f);
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throttle_control = constrain_float(throttle_control,0.0f,1000.0f);
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// ensure a reasonable deadzone
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g.throttle_deadzone = constrain_int16(g.throttle_deadzone, 0, 400);
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@ -185,7 +184,7 @@ float Copter::get_pilot_desired_climb_rate(float throttle_control)
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// check throttle is above, below or in the deadband
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if (throttle_control < deadband_bottom) {
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// below the deadband
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desired_rate = g.pilot_velocity_z_max * (throttle_control-deadband_bottom) / (deadband_bottom-g.throttle_min);
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desired_rate = g.pilot_velocity_z_max * (throttle_control-deadband_bottom) / deadband_bottom;
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}else if (throttle_control > deadband_top) {
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// above the deadband
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desired_rate = g.pilot_velocity_z_max * (throttle_control-deadband_top) / (1000.0f-deadband_top);
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