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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Self-adaptive missile guidance system for statistical inputs


    Additional title:

    NASA -- Tech Note


    Contributors:
    Peery, H.R. (author)


    Publication date :

    1960


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English







    Synthesis of optimum homing missile guidance systems with statistical inputs

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


    Missile guidance system against a ballistic missile

    BABA, YORIAKI / TAKANO, HIROYUKI / TAKAO, KICHIRO | AIAA | 1991