Electrotor-SloMo - Control Flight - Aerodynamic Twist

Objectives:

  1. To reduce the forces from the pilot when applying pitch and roll change by weight-shift, while allowing for a reasonably large rotor disk area for lower power input for a given thrust and a slower descent rate in autorotation.
  2. To reduce the effect of external perturbations by providing a short-term opposing pitch change to the tip of the blades.

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B621

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Electrotor-SloMo - Control - Flight - Aerodynamic Twist - Overview

2003

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Initially displayed: May 11, 2010 ~ Last Revised: April 15, 2012