Paper considers design of simplified beam-rider missile guidance system where inputs are known in statistical sense, where saturation exists, and open-loop gain changes as function of dynamic pressure; method is presented for designing systems that will automatically adjust Wiener filter part of guidance system as function of percent of time of acceleration limiting.


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    Titel :

    Self-adaptive missile guidance system for statistical inputs


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Peery, H.R. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :





    Synthesis of optimum homing missile guidance systems with statistical inputs

    Stewart, E.C. / Smith, G.L. | Engineering Index Backfile | 1959


    Missile guidance

    Felch, E.P. | Engineering Index Backfile | 1959