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    Title :

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



    Conference:

    Conference, Guidance, navigation and control; AIAA guidance ; 2013 ; Boston, MA



    Publication date :

    2013-01-01


    Size :

    12 pages


    Remarks:

    Includes bibliographical references and index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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