A new scheme of Reaction-jet/Aerodynamic Multi-control missile using pose controlled pulse-engine is present. In this scheme Aerodynamic is used as feedback control, and Reaction-jet is feed-forward control. In the first part, the model of the multi-control system is given; then, the Aerodynamic controller is designed by using pole assignment, and the Reaction-jet controller has been designed by using the term of entirely compensated. Finally it has been proved by simulation that this multiple controller can greatly enhance response speed and the scheme is feasible.


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    Title :

    Design of Autopilot for Aerodynamic/Reaction-Jet Multiple Control Missile


    Contributors:
    Sui, Qi SHeng (author) / Li, Xin (author) / Fan, Yong Hua (author)


    Publication date :

    2008-10-01


    Size :

    175061 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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