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    Titel :

    Using the State-Dependent Riccati Equation and Kalman Filter Techniques to Design a Satellite Attitude Control Simulator (IAA-AAS-DyCoSS1-07-09 - AAS 12-351)



    Kongress:

    Conference, Dynamics and Control of Space Systems; proceedings of the 1st International Academy of Astronautics Conference ; 2012 ; Porto, Portugal



    Erscheinungsdatum :

    01.01.2012


    Format / Umfang :

    14 pages


    Anmerkungen:

    Includes bibliographical references and indexes; ALSO HELD ON CD-ROM




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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