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FIBER OPTIC SENSING AND CONTROL SYSTEM

  • US 20170021914A1
  • Filed: 12/08/2014
  • Published: 01/26/2017
  • Est. Priority Date: 12/11/2013
  • Status: Abandoned Application
First Claim
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1. An aeronautical control system comprising:

  • a flight control surface of an aircraft or spacecraft;

    a first optical fiber;

    said first optical fiber having a fiber optic sensor configured and arranged to sense a first parameter associated with said flight control surface at a first position and a second fiber optic sensor configured and arranged to sense a second parameter associated with said flight control surface at a second location;

    an interrogator connected to said first optical fiber and configured and arranged to convert said sensed parameters from both said first fiber optic sensor and said second fiber optic sensor into an electrical signal; and

    said interrogator communicating with a flight control computer.

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