Paper
14 October 1996 Long stroke optical fiber linear position sensor for the FLASH program
Robert D. LaClair, William B. Spillman Jr., W. W. Kuhns, Mark S. Miller
Author Affiliations +
Abstract
The DARPA Fly-by-Light Advanced System Hardware (FLASH) program is aimed at practical fiber optic component development for next generation aerospace systems. For aircraft control, large numbers of linear position sensors are generally needed on the vehicle. In particular, these are needed for closed loop control of flight surfaces in which the sensor continuously monitors actuator position in order to provide feedback to the control system. In this paper, we briefly describe the principle of operation, design and operational characteristics of a long stroke length (20 cm, 7.9 inches) wavelength encoding multimode fiber optic linear position sensor developed for the FLASH program.
© (1996) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Robert D. LaClair, William B. Spillman Jr., W. W. Kuhns, and Mark S. Miller "Long stroke optical fiber linear position sensor for the FLASH program", Proc. SPIE 2840, Fly-by-Light III, (14 October 1996); https://doi.org/10.1117/12.254223
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Cited by 4 scholarly publications.
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KEYWORDS
Sensors

Diffraction gratings

Position sensors

Actuators

Aerospace engineering

Iron

Mirrors

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