The flight control system design method of wing-in-ground effect aircraft is presented based on robust control theory. With a view to uncertainty of lengthways channels, the simplified mathematical model is constituted for wing-in-ground effect aircraft. According to this simplified model, the lengthways control system is designed. In order to overcome defect of uncertain system, the flight controller of wing-in-ground effect aircraft is designed using robust control theory. Simulation results show that this control method can implement efficiently precision control mission for wing-in-ground effect aircraft as well as preferable robustness.


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    Titel :

    Robust design method for flight control system of cruise missile


    Beteiligte:
    Yongxin Yin, (Autor:in) / Zhongming Ou, (Autor:in) / Wen Shi, (Autor:in)


    Erscheinungsdatum :

    01.06.2010


    Format / Umfang :

    846495 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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