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


    Contributors:
    Dorsky, L. (author) / Bartman, R. (author) / Lehman, D. (author) / Salomon, P. (author) / Freier, L. (author) / Laznicka, O. (author) / Magee, R. (author) / Murphy, J. (author)


    Publication date :

    1992-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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