Paper
3 February 1999 Development of fiber optic sensors for advanced aircraft testing and control
Scott A. Meller, Mark E. Jones, Thomas A. Wavering, Carrie L. Kozikowski, Kent A. Murphy
Author Affiliations +
Abstract
Optical fiber sensors, because of the 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 design for monitoring acceleration on aircraft. Flight testing of the final accelerometer design will be conducted on the F-18 Systems Research Aircraft at NASA Dryden Flight Research Center in Edwards, CA.
© (1999) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Scott A. Meller, Mark E. Jones, Thomas A. Wavering, Carrie L. Kozikowski, and Kent A. Murphy "Development of fiber optic sensors for advanced aircraft testing and control", Proc. SPIE 3541, Fiber Optic and Laser Sensors and Applications; Including Distributed and Multiplexed Fiber Optic Sensors VII, (3 February 1999); https://doi.org/10.1117/12.339085
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CITATIONS
Cited by 3 scholarly publications.
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KEYWORDS
Fiber optics sensors

Sensors

Fiber optics

Control systems

Reflection

Temperature metrology

Demodulation

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