In this paper the attitude control system of a small spacecraft is considered. The readings of airborne magnetometers and satellite Global Positioning System (GPS) data are used for determination of the parameters of object motion. Such choice of measurements aims to raise estimation stability against disturbances of the magnetic storm type. At considerably undefined initial conditions for estimation of the desired parameters of motion, we use the algorithm with an extended convergence domain.


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    Title :

    Spacecraft attitude control using the magnetic-GPS dataware system. I


    Contributors:


    Publication date :

    2001


    Size :

    7 Seiten, 20 Quellen



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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