Instantaneous three-axis attitude control in many picoscale satellites is achieved by combining magnetic torque coils with other control devices such as thrusters. A B-spline augmented virtual motion camouflage method is presented to maximize the usage of magnetic torque coils and minimize that of thrusters, while calculating attitude guidance commands.


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    Titel :

    Optimal attitude control allocation via the B-spline augmented virtual motion camouflage method


    Beteiligte:
    Develle, Mike (Autor:in) / Xu, Yunjun (Autor:in)


    Erscheinungsdatum :

    01.07.2015


    Format / Umfang :

    764696 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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