In this paper, a maneuver controller for a nonlinear six-degree-of-freedom aircraft is designed, which makes angle-of-attack, sideslip angle, and roll rate asymptotically track the reference trajectories respectively. The design procedures for angle-of-attack and sideslip angle are based on backstepping method. Appropriate cost functions for angle-of-attack and sideslip angle are constructed to satisfy Hamilton-Jacobi-Isaacs (HJI) equations, thereby the tracking of the angle-of-attack and the sideslip angle attains a desired disturbance attenuation level. Simulation results on a nonlinear aircraft model are given to illustrate the performance of the maneuver controller.


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    Title :

    A maneuver controller with disturbance attenuation for aircraft


    Contributors:
    Ruyi Yuan, (author) / Jianqiang Yi, (author) / Guoliang Fan, (author) / Wensheng Yu, (author) / Liwei Qiu, (author)


    Publication date :

    2010-06-01


    Size :

    600643 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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