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    Title :

    Optimal Control of Spacecraft Orbital Maneuvers by the Hamilton-Jacobi Theory


    Contributors:

    Conference:

    AIAA Guidance, Navigation, and Control Conference and Exhibit



    Publication date :

    2006-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    AIAA-2006-6234 Optimal Control of Spacecraft Orbital Maneuvers by the Hamilton-Jacobi Theory

    Park, C. / Scheeres, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006





    Optimal Nonlinear Spacecraft Attitude Control Through Hamilton-Jacobi Formulation (AAS 01-383)

    Tewari, A. / AAS / AIAA | British Library Conference Proceedings | 2001