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.
Fiber optic rotation sensor for long lifetime space missions
Controls for Optical Systems ; 1992 ; Orlando,FL,United States
Proc. SPIE ; 1696
1992-07-10
Conference paper
Electronic Resource
English
Fiber optic rotation sensor for long lifetime space missions
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