Testing system studies inertial characteristics of gyroscopic devices. System consisting of instrument support package, dynamic test table, torque control electronics, and real-time computer evaluates performance of prototype gyroscopic strapdown units in inertial-grade attitude-reference systems. System is applicable to commercial aircraft.


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    Title :

    Performance evaluation system for inertial navigation equipment


    Contributors:

    Publication date :

    1971-04-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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