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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Robust design method for flight control system of cruise missile


    Contributors:
    Yongxin Yin, (author) / Zhongming Ou, (author) / Wen Shi, (author)


    Publication date :

    2010-06-01


    Size :

    846495 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Cruise missile system design

    LOCKE, W. | AIAA | 1981


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

    Yuan, Xiao Dong ;Gao, Shi Qiao | Trans Tech Publications | 2012




    Environmental control system design for the Tomahawk Cruise Missile

    Walburn, A.B. / Dupont, H.M. | Tema Archive | 1979