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    Title :

    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)



    Conference:

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



    Publication date :

    2012-01-01


    Size :

    14 pages


    Remarks:

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




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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