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Integrated optics implementation of a fiber optic rotation sensor - Analysis and developmentThe Jet Propulsion Laboratory is developing a fiber optic rotation sensor (FORS) for use on the Mariner Mark II series of planetary explorer craft and in other space applications. FORS is a closed-loop phase-nulling device and embodies a number of interesting innovations. Chief among these are the incorporation of the device's couplers, phase modulators, and polarizer on a single lithium niobate (LinbO3) integrate optics chip and a novel means of reading out angular position and rotation rate based on optical beat detection. Various aspects of the FORS design and operation are described and discussed. Particular attention is paid to analyzing errors attributable to polarizer imperfection and the so-called residual Michelson effect.
Document ID
19880036985
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bartman, R. K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Youmans, B. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Nerheim, N. M.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Instrumentation
Accession Number
88A24212
Distribution Limits
Public
Copyright
Other

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