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    Title :

    Optimal Feedback Guidance for Nonlinear Missile Model with Impact Time and Angle Constraints


    Contributors:

    Conference:

    AIAA Guidance, Navigation, and Control (GNC) Conference



    Publication date :

    2013-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Optimal Feedback Guidance for Nonlinear Missile Model with Impact Time and Angle Constraints (AIAA 2013-4785)

    Arita, S. / Ueno, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013



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