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    Landing Control System Design for a Flying-Wing Aircraft Based on ADRC

    Landing Control System Design for a Flying-Wing Aircraft Based on ADRC


    In this paper, the flight simulation and control of a flying-wing aircraft in landing is presented. Significant dynamic nonlinearity and atmospheric disturbance are main problems for a flying-wing aircraft in landing phase. Therefore, a nonlinear controller with strong robustness is required. Active disturbance rejection control technique is used to design the controller which could estimate and compensate the uncertainties. A landing condition in which the wind shear encounters and ground effect before touchdown is considered, and a nonlinear longitudinal dynamic model of flying-wing aircraft in variable wind field is established. Simulations are conducted in MATLAB and the controller is shown to suppress the wind effects and ground proximity.

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    Titel :

    Landing Control System Design for a Flying-Wing Aircraft Based on ADRC

    Beteiligte:
    Wang, Yanxiong (Autor:in) / Zhu, Xiaoping (Autor:in) / Zhou, Zhou (Autor:in) / Shao, Zhuang (Autor:in)
    Erschienen in:

    ICIRA, International Conference on Intelligent Robotics and Applications, 7 ; 340-351

    Lecture Notes in Computer Science, Lecture Notes in Artificial Intelligence ; 8917

    Erscheinungsdatum :

    2014

    Format / Umfang :

    12 Seiten

    ISBN :

    978-3-319-13966-1 , 978-3-319-13965-4

    ISSN :

    0302-9743

    DOI :

    https://doi.org/10.1007/978-3-319-13966-1_34

    Medientyp :

    Aufsatz (Konferenz)

    Format :

    Print

    Sprache :

    Englisch

    Schlagwörter :

    nichtlineare Regelung , Bodeneffekt , Informatik , Rechneranwendung , Luftfahrzeug , Mustererkennung , Flugsimulation , Robotik , Regelungssystementwurf , atmosphärische Störung , Nichtlinearität , dynamisches Modell , Regelungstechnik

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