The guidance and control problem for tactical air-to-air missiles is addressed using a modern control theory approach. The autopilot is designed based upon a generalized formulation of the optimal tracker to provide both airframe stability and command following from the guidance signals, and the guidance law is designed using the optimal regulator. Associated implementation issues are discussed.


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    Title :

    An integrated approach to the guidance and control of tactical missiles


    Additional title:

    Eine integrierte Loesung zur Fuehrung und Steuerung von taktischen Flugkoerpern


    Contributors:


    Publication date :

    1983


    Size :

    6 Seiten, 2 Bilder, 3 Tabellen, 7 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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