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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    Title :

    Fiber optic rotation sensor for long lifetime space missions



    Conference:

    Controls for Optical Systems ; 1992 ; Orlando,FL,United States


    Published in:

    Publication date :

    1992-07-10





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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