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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    Title :

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


    Contributors:
    Develle, Mike (author) / Xu, Yunjun (author)


    Publication date :

    2015-07-01


    Size :

    764696 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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