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    Title :

    Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method


    Contributors:

    Conference:

    Conference, Nonlinear problems in aviation and aerospace ; 2000 ; Daytona Beach, FL



    Publication date :

    1999-01-01


    Size :

    20 pages




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English