Attitude control devices used to dampen vehicle librations are single-degree-of-freedom integrating gyros, called control moment gyros (CMG), which control vehicle to orbital reference established by earth-to-satellite radius vector and orbital angular momentum vector; design parameters; CMG control system is optimized, using Monte Carlo techniques, and results of optimization are shown; optimization technique and its utility; linearization techniques, their limitations, and example showing where linearization can produce serious errors in system analysis.


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    Title :

    Control moment gyro gravity stabilization


    Additional title:

    Progress Astronautics Aeronautics


    Contributors:
    Scott, E.D. (author)


    Publication date :

    1964


    Size :

    46 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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