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Proceedings Paper

Development of fiber optic gyroscope with environmental ruggedness
Author(s): Aritaka Ohno; Shinji Motohara; Ryuji Usui; Yuji Itoh; Kenichi Okada
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Paper Abstract

The present investigation of FOG behavior under vibration conditions gives attention to effective techniques for vibration-compensation. The FOGs tested are noted to yield an intermediate level of performance, of the order of 3 deg/hr at 1-sigma, under commonly encountered vibration conditions and over the temperature range associated with aerospace applications. These FOGs have been deemed adequate for use in the triaxial inertial devices of the guidance and control system aboard the TR-1 rocket.

Paper Details

Date Published: 1 February 1992
PDF: 7 pages
Proc. SPIE 1585, Fiber Optic Gyros: 15th Anniversary Conf, (1 February 1992); doi: 10.1117/12.135037
Show Author Affiliations
Aritaka Ohno, Japan Aviation Electronics Industry, Ltd. (Japan)
Shinji Motohara, Japan Aviation Electronics Industry, Ltd. (Japan)
Ryuji Usui, Japan Aviation Electronics Industry, Ltd. (Japan)
Yuji Itoh, Japan Aviation Electronics Industry, Ltd. (Japan)
Kenichi Okada, Japan Aviation Electronics Industry, Ltd. (Japan)


Published in SPIE Proceedings Vol. 1585:
Fiber Optic Gyros: 15th Anniversary Conf

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