Wavelength Division Multiplexed Fiber Optic Sensors For Aircraft Applications

Norris E. Lewis; Michael B. Miller

doi:10.1117/12.963216

13 February 1990 Wavelength Division Multiplexed Fiber Optic Sensors For Aircraft Applications

Norris E. Lewis, Michael B. Miller

Proceedings Volume 1173, Fiber Optic Systems for Mobile Platforms III; (1990) https://doi.org/10.1117/12.963216
Event: OE/FIBERS '89, 1989, Boston, United States

Abstract

This paper describes the design and performance of a rotary position sensor system based on the principle of wavelength division multiplexing. The system is discussed in relation to the requirements on the source, sensor and detection circuits. Measured performance of the various components is presented for environmental conditions typical of various application areas within the aircraft. The wavelength sensing technique becomes the basis for an electro-optic architecture capable of multiplexing several sensors onto one common interface.

Citation Download Citation

Norris E. Lewis and Michael B. Miller "Wavelength Division Multiplexed Fiber Optic Sensors For Aircraft Applications", Proc. SPIE 1173, Fiber Optic Systems for Mobile Platforms III, (13 February 1990); https://doi.org/10.1117/12.963216

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