A variable-structure control approach is presented for multiaxial spacecraft attitude maneuvers. Nonlinear sliding surfaces are proposed that result in asymptotically stable, ideal linear decoupled sliding motions of Cayley-Rodrigues attitude parameters, as well as of angular velocities. The resulting control laws are interpreted as more easily implemented and more robust versions of those previously obtained by feedback linearization.


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    Title :

    Variable-structure control of spacecraft attitude maneuvers


    Contributors:


    Publication date :

    1988-06-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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