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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    Titel :

    Fiber optic rotation sensor for long lifetime space missions


    Beteiligte:
    Dorsky, Leonard I. (Autor:in) / Bartman, Randall K. (Autor:in) / Lehman, David H. (Autor:in) / Salomon, Phil M. (Autor:in) / Freier, Larry J. (Autor:in) / Laznicka, Oldrich M. (Autor:in) / Magee, R. (Autor:in) / Murphy, J. (Autor:in)

    Kongress:

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


    Erschienen in:

    Erscheinungsdatum :

    10.07.1992





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Fiber optic rotation sensor for long lifetime space missions

    Dorsky, L. / Bartman, R. / Lehman, D. et al. | NTRS | 1992


    Fiber optic rotation sensor for long lifetime space missions

    Dorsky, L. / Bartman, R. / Lehman, D. et al. | Tema Archiv | 1992


    Fiber optic rotation sensor for space missions

    De Paula, R. P. / Bartman, R. K. / Youmans, B. R. et al. | NTRS | 1988


    Fiber Optic Rotation Sensor For Space Missions

    De Paula, R . P. / Minford, W. J. / Bartman, R. K. et al. | SPIE | 1988


    Fiber optic sensors for space missions

    Benussi, L. / Berardis, S. / Bertani, M. et al. | IEEE | 2003