An adaptive control scheme for the attitude control of a rigid spacecraft is derived using a linear parameterization of the equation of motion. The tracking error is described with the Euler parameter vector. Global convergence of the tracking error to zero is shown using passivity theory. This allows for the use of time-varying positive-definite feedback gain matrices, and the results can easily be extended to other passive parameter update laws.


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    Title :

    Passivity-based adaptive attitude control of a rigid spacecraft


    Additional title:

    Passivitätsbasierte adaptive Fluglagenregelung eines starren Raumfahrzeugs


    Contributors:
    Egeland, O. (author) / Godhavn, J.M. (author)

    Published in:

    Publication date :

    1994


    Size :

    5 Seiten, 2 Bilder, 16 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English