Separation section is the most complex and dramatic stage in disturbing the cruise missile during the entire flight trajectory. The characteristic of low-altitude, low-speed, non-aileron flight separation of the missile propelled by rocket was analyzed in this paper. Classic engineering methods and neural network dynamic inversion methods was used to design control system, and two different control methods were compared.


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    Title :

    One Kind of Flight Control System Design for Separation Section in Cruise Missile



    Published in:

    Advanced Materials Research ; 490-495 ; 885-889


    Publication date :

    2012-03-15


    Size :

    5 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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