Dynamic equations of motion are developed which describe the rotational motion for a large space structure having rotating appendages. The presence of the appendages produce torque coupling terms which are dependent on the inertia properties of the appendages and the rotational rates for both the space structure and the appendages. These equations were formulated to incorporate into the Space Station Attitude Control and Stabilization Test Bed to accurately describe the influence rotating solar arrays and thermal radiators have on the dynamic behavior of the Space Station.


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    Title :

    Space Station Rotational Equations of Motion


    Contributors:

    Publication date :

    1985


    Size :

    21 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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