NASA NTRS · 19780000176
Optical gyroscope
Abstract
Instrument uses phase difference between two beams of light to measure rotation. It is considerably simpler and more reliable than conventional spinning-mass gyroscopes used for inertial guidance and is more compact, lighter, and potentially less expensive. Moreover, optical gyroscope requires no warmup period. Although conceived for spacecraft and satellite stabilization, gyroscope should also find applications in flight instruments for private, commercial, and military aircraft.
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Goldstein, R. M., Goss, W. C.. 1978-10-01. Optical gyroscope. https://ntrs.nasa.gov/citations/19780000176
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