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, L. (Autor:in) / Bartman, R. (Autor:in) / Lehman, D. (Autor:in) / Salomon, P. (Autor:in) / Freier, L. (Autor:in) / Laznicka, O. (Autor:in) / Magee, R. (Autor:in) / Murphy, J. (Autor:in)


    Erscheinungsdatum :

    01.01.1992


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Dorsky, Leonard I. / Bartman, Randall K. / Lehman, David H. et al. | SPIE | 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