Parameter variation and load disturbance will have great influence on the performance of missile electromechanical actuator system and further on the performance of the entire missile system during the missile flight process. To solve this problem, a variable structure control system for missile electromechanical actuator system was proposed in this paper. To verify the proposed control scheme, simulation has been performed for different system parameters. Simulation results indicate that the proposed variable structure control method can provide the properties of robustness to load and environment disturbance and insensibility to parameter variation. So it is very suitable for complicated and variable flight environment of missile.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Application of Variable Structure Control in Missile Electromechanical Actuator System


    Contributors:
    Gao, Yuan (author) / Gu, Liang-xian (author) / Pan, Lei (author)


    Publication date :

    2008-10-01


    Size :

    274919 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Discrete Adaptive Global Sliding Mode Control for Missile Electromechanical Actuator System

    Liu, X. / Wu, Y. / Zhang, W. et al. | British Library Online Contents | 2013


    A global sliding mode controller for missile electromechanical actuator servo system

    Liu, Xiaodong / Wu, Yunjie / Deng, Yong et al. | SAGE Publications | 2014



    Sliding Mode Variable Structure Control for Electromechanical Actuator with Nonlinear Friction

    Peng, S.-h. / Li, H.-d. / Su, Z. | British Library Online Contents | 2008


    MULTIPLE ELECTROMECHANICAL ACTUATOR CONTROL SYSTEM

    PECK JAMES L JR / QUIAMBAO JIMMY M / COFFMAN JEFFREY CHARLES | European Patent Office | 2018

    Free access