RC Helicopter - Autorotation Inverted

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The slider controls have been adjusted to increase the rate at which the RPM increases, and to increase the maximum RPM that can be reached.

The drag factor caused by cyclic and collective pitch changes has also been reduced to help prolong the blades spinning.

Additional autorotation demonstrations can be found here: https://www.rcsimanic.com/video-collection/autorotation-landing.php