Fiber optic rotation sensor for long lifetime space missions

Details Fiber optic rotation sensor for long lifetime space missions Fiber optic rotation sensor for long lifetime space missions

Jul 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992spie.1696...27d&link_type=abstract

In: Controls for optical systems; Proceedings of the Meeting, Orlando, FL, Apr. 21, 22, 1992 (A93-34276 13-74), p. 27-40.

Physics

Optics

Electro-Optics, Fiber Optics, Laser Gyroscopes, Long Duration Space Flight, Optical Measuring Instruments, Angular Velocity, Cost Reduction, Ring Lasers, Solid State Devices

Scientific paper

The present F-O rotation sensors (FORS) are all-solid state devices for measuring rotations and rotation rates in inertial space that may reach the 0.003 deg/hr (1-sigma) accuracies required for NASA's Saturn-orbiting Cassini mission. Attention is presently given to the mission, inertial reference unit, and FORS instrument optoelectronic component requirements envisioned for such spacecraft applications.

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