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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    Title :

    Development of fiber optic gyroscope with environmental ruggedness


    Contributors:

    Conference:

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


    Published in:

    Proc. SPIE ; 1585 ; 82


    Publication date :

    1992-02-01





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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