Analysis is presented of means of decoupling gyro bias associated with rate gyro, to make sure missile autopilot performance is not depreciated significantly. From Kansas State Univ Bul v 47 n 9.


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    Title :

    Elimination of steering rate gyro bias in missile autopilot


    Additional title:

    Simulation


    Contributors:

    Published in:

    Simulation ; 2 , n 1


    Publication date :

    1964


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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