A terminal sliding mode controller is designed for a generic air-breathing hypersonic vehicles (AHVs). The model of AHVs is nonlinear, and includes uncertain parameters and intricate coupling between the engine and flight dynamics. An affine form of the longitudinal model is obtained by input/output linearization, and then a controller is designed by using terminal sliding mode method. The terminal sliding mode can make the system stabilize in finite time. Simulation results are provided to show the availability of the designed controller by excellent altitude and velocity tracking performance.


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    Title :

    Terminal sliding mode control design for air-breathing hypersonic vehicles


    Contributors:
    Xiaoxiang Hu, (author) / Changxing Ding, (author) / Ligang Wu, (author) / Changhua Hu, (author) / Hongyi Li, (author) / Yulin Si, (author) / Zeguo Wang, (author)


    Publication date :

    2010-06-01


    Size :

    790313 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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