A model reference adaptive control law is presented for largeangle rotational maneuvers of spacecraft using reaction jets. It isassumed that the various parameters of the spacecraft arecompletely unknown, and unknown but bounded disturbancetorques are acting on the spacecraft. The controller includes adynamic system in the feedback path. Simulation results arepresented to show that fast, large angle rotational maneuvers can beperformed using the adaptive controller in spite of uncertainty inthe system.


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    Titel :

    Nonlinear Adaptive Attitude Control of Spacecraft


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1987-05-01


    Format / Umfang :

    1977800 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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    Singh, Sahjendra N. | NTRS | 1987


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