Stability characteristics are described for four gimbal inertial platforms installed on vehicles to provide fixed attitude reference system; platform stabilization criteria are formulated that relate arbitrary vehicle maneuvers to ratio of available motor torque to gimbal inertial reaction, dynamics of inner roll gimbal angle when outer roll servo loop operates below and at motor torque saturation, and vehicle angular acceleration stability regions; analysis provides method to determine required ratio of motor torque to gimbal inertia reaction as function of vehicle motion and gimbal orientation.


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    Title :

    Inertial platform stabilization criteria for arbitrary vehicle maneuvers


    Additional title:

    J Aircraft


    Contributors:
    Hanisch, B. (author)

    Published in:

    Publication date :

    1967


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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