This report briefly reviews the principles of optical rate sensors. It then further describes some existing ring laser gyro systems and considers how their utilization would affect performance, cost and reliability of attitude control systems currently used or proposed for use in sounding rocket applications at the Air Force Geophysics Laboratory (AFGL).


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Laser Gyro Attitude Control System Feasibility


    Beteiligte:
    C. R. Cassell (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    41 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    COAXIAL TWIN-GYRO ATTITUDE CONTROL SYSTEM

    LEE HYUCK SIK | Europäisches Patentamt | 2018

    Freier Zugriff

    A Feasibility Study on Attitude Filtering without Rate Gyro

    Ma, Hongliang / Chen, Tong / Huang, Xiangyu et al. | AIAA | 2012


    A Feasibility Study on Attitude Filtering without Rate Gyro

    Ma, H. / Chen, T. / Huang, X. et al. | British Library Conference Proceedings | 2012


    Twin-gyro attitude control systems.

    HUSTON, R. L. | AIAA | 1966


    GYRO STELLAR ATTITUDE DETERMINATION

    Ghezal, M. / Polle, B. / Rabejac, C. et al. | British Library Conference Proceedings | 2006