A new method for attitude fuzzy control has been presented for the interceptor by combined control of lateral thrust and aerodynamic force, and the torque received by interceptor has been analyzed, and the influences of jet have been described, models of the attitude motion have been constructed, and the new method for attitude fuzzy control has been presented, which is simple and is convenient for practical project. The simulation results show that this method can fleetly and effectual come true attitude control of the interceptor, and shows that these models have higher control precision, and shows the advantage of the method.


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    Titel :

    Research on the method for attitude fuzzy control of the interceptor


    Beteiligte:
    Yongxin Yin, (Autor:in) / Ming Yang, (Autor:in) / Zicai Wang, (Autor:in)


    Erscheinungsdatum :

    2006-01-01


    Format / Umfang :

    3986024 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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