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FULL AUTHORITY FLY-BY-WIRE PEDAL SYSTEM

  • US 20100078524A1
  • Filed: 12/01/2009
  • Published: 04/01/2010
  • Est. Priority Date: 02/15/2006
  • Status: Active Grant
First Claim
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1. A method of controlling a yaw axis of a rotary-wing aircraft comprising the steps of:

  • (A) maintaining stability and coordination through a fly-by-wire flight control system;

    and(B) receiving a pilot yaw control input only when a change in a yaw axis state is demanded, the pilot yaw control input provided through a double gradient force feedback pedal dynamic for control of an anti-torque system.

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