Experimental optimal relay guidance system to control bang-bang, line of sight guidance missile is described; it makes use of both instantaneous pilot commands and past history of commands in order to derive missile maneuver orders which are based on more optimal strategy; proper error nulling is aided by injecting anticipatory synthetic missile dynamics which tend to damp out phase lags and other interactions associated with human and missile aerodynamics.


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    Titel :

    Optimal bang-bang guidance system


    Weitere Titelangaben:

    WESCON Convention Rec


    Beteiligte:
    Harmon, G.L. (Autor:in) / Kent, K.E. (Autor:in) / Purcell, W.O. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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