Development Of Fiber Optic Sensors For Advanced Aircraft Testing And Controls

S. A. Meller,M. E. Jones,T. A. Wavering,C. L. Kozikowski,K. A. Murphy

FIBER OPTIC AND LASER SENSORS AND APPLICATIONS: INCLUDING DISTRIBUTED AND MULTIPLEXED FIBER OPTIC SENSORS VII（1999）

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Abstract

Optical fiber sensors, because of their small size, low weight, extremely high information carrying capability, immunity to electromagnetic interference, and large operational temperature range, provide numerous advantages over conventional electrically based sensors. This paper presents preliminary results from optical fiber sensor designs for monitoring acceleration on aircraft. Flight testing of the final accelerometer design will be conducted on the F-18 Systems Research Aircraft (SRA) at NASA Dryden Flight Research Center in Edwards, CA.

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Key words

optical fiber sensors, extrinsic Fabry-Perot interferometer, acceleration

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