The following topics are discussed: (1) modeling of articulated spacecraft as multi-flex-body systems; (2) nonlinear attitude control by adaptive partial feedback linearizing (PFL) control; (3) attitude dynamics and control for SSF/MRMS; and (4) performance analysis results for attitude control of SSF/MRMS.


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    Title :

    Case Study in Nonlinear Dynamics and Control of Articulated Spacecraft: The Space Station Freedom with a Mobile Remote Manipulator System


    Contributors:
    W. H. Bennett (author) / H. G. Kwatny (author) / C. Lavigna (author) / G. Blankenship (author)

    Publication date :

    1994


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English