Application of optimal control and filtering theory to controller design for a bank-to-turn missile operating under CLOS guidance is described. One approach is based on two identical single-plane compensators. The second problem fromulation involves direct choice of lift force magnitude and orientation. The effect of constraining the roll rate is discussed for both fixed-and variable-wing-angle configurations.


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    Title :

    Design of controllers for bank-to-turn CLOS guidance using optimal control


    Additional title:

    Entwurf von Reglern fuer optimale Steuerung von Kurzstreckenraketen


    Contributors:
    Irwin, G.W. (author)

    Published in:

    Publication date :

    1986


    Size :

    6 Seiten, 7 Bilder, 2 Tabellen, 7 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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