The study of a one-on-one aircraft pursuit-evasion guidance scheme for high-performance aircraft is discussed. The research objective is to implement a guidance law derived earlier using differential game theory in conjunction with the theory of feedback linearization. Unlike earlier research in this area, the present formulation explicitly recognizes the two-sided nature of the pursuit-evasion scenario. The present research implements the guidance law in a realistic model of a modern high-performance fighter aircraft. Also discussed are the details of the guidance law, implementation in a highly detailed simulation of a high-performance fighter, and numerical results for two engagement geometries. Modifications of the guidance law for onboard implementation is also discussed.


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    Title :

    Study of a pursuit-evasion guidance law for high performance aircraft


    Contributors:

    Conference:

    1989 American Control Conference ; 1989 ; Pittsburgh, PA, United States


    Publication date :

    1989-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English






    Pursuit-evasion between two realistic aircraft

    HILLBERG, C. / JAERMARK, B. | AIAA | 1983


    Pursuit-evasion between two realistic aircraft

    JARMARK, B. / HILLBERG, C. | AIAA | 1984