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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    Titel :

    Synthesis of optimum homing missile guidance systems with statistical inputs


    Weitere Titelangaben:

    NASA Memo


    Beteiligte:
    Stewart, E.C. (Autor:in) / Smith, G.L. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    57 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Optically aided homing missile guidance

    Andrisani, ck, II, Dominick, | AIAA | 1995


    Final-value homing missile guidance.

    ABZUG, M. J. | AIAA | 1967


    Information Enhancement and Homing Missile Guidance

    J. L. Speyer / D. G. Hull | NTIS | 1982


    Guidance and control for homing missile

    Engineering Index Backfile | 1958