The present investigation of FOG behavior under vibration conditions gives attention to effective techniques for vibration-compensation. The FOGs tested are noted to yield an intermediate level of performance, of the order of 3 deg/hr at 1-sigma, under commonly encountered vibration conditions and over the temperature range associated with aerospace applications. These FOGs have been deemed adequate for use in the triaxial inertial devices of the guidance and control system aboard the TR-1 rocket.


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    Titel :

    Development of fiber optic gyroscope with environmental ruggedness


    Beteiligte:
    Ohno, Aritaka (Autor:in) / Motohara, Shinji (Autor:in) / Usui, Ryuji (Autor:in) / Itoh, Yuji (Autor:in) / Okada, Kenichi (Autor:in)

    Kongress:

    Fiber Optic Gyros: 15th Anniversary Conf ; 1991 ; Boston,MA,United States


    Erschienen in:

    Proc. SPIE ; 1585 ; 82


    Erscheinungsdatum :

    01.02.1992





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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