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ACTUATOR CONTROL SYSTEM

  • US 20140172203A1
  • Filed: 03/22/2012
  • Published: 06/19/2014
  • Est. Priority Date: 03/29/2011
  • Status: Active Grant
First Claim
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1. An actuator control system for coupling to one or more flight control computers, flight control computers hereinafter being referred to as FCCs;

  • the actuator control system comprising;

    apparatus for controlling an aerodynamic control surface in response to commands received from one or more FCCs, and, integrated with the controlling apparatus, a failure protection system comprising apparatus arranged to provide at least one of the following functionalities;

    a servo monitor functionality, a command monitor functionality, and a loop closure functionality.

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