Analytical approach presented is applicable to optimization of systems operating in presence of radar noise; factors considered are target evasive maneuver, radar glint noise, missile maneuverability, and inherent time varying character of kinematics; method of finding approximate solutions utilizing time varying control systems.


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    Title :

    Synthesis of optimum homing missile guidance systems with statistical inputs


    Additional title:

    NASA Memo


    Contributors:
    Stewart, E.C. (author) / Smith, G.L. (author)


    Publication date :

    1959


    Size :

    57 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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