Active center of gravity (C.G.) control is a key technology of vehicle management system, which has been extensively used in various types of aircraft. With active C.G. control system, aircraft may deviate from its known dynamics due to the C.G. offset, thus bringing new problems to the existing flight control system. A new design approach of the attitude control system of aircraft with C.G. variations is proposed in this paper.


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    Titel :

    Modeling and attitude control of aircraft with center of gravity variations


    Beteiligte:
    Jing Zhang, (Autor:in) / Lingyu Yang, (Autor:in) / Gongzhang Shen, (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.03.2009


    Format / Umfang :

    342374 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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