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NASA NTRS ยท 19730016736

Interferometric rotation sensor

Abstract

An interferometric rotation sensor and control system is provided which includes a compound prism interferometer and an associated direction control system. Light entering the interferometer is split into two paths with the light in the respective paths being reflected an unequal number of times, and then being recombined at an exit aperture in phase differing relationships. Incoming light is deviated from the optical axis of the device by an angle, alpha. The angle causes a similar displacement of the two component images at the exit aperture which results in a fringe pattern. Fringe numbers are directly related to angle alpha. Various control systems of the interferometer are given.

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BibTeXRIS

Walsh, T. M.. 1973-04-24. Interferometric rotation sensor. https://ntrs.nasa.gov/citations/19730016736

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