The purpose of this paper is to introduce a complex nonlinear model to a novel tandem ducted fan vehicle which adopted a structure of coaxial rotor and cyclic pitch system, considering aerodynamic coupling, disturbing between the upper and the lower rotor, and special aerodynamic characteristics of duct. On this basis, a robust hover control system has been designed to attitude control using H-infinite static output feedback theory. The results illustrate that the system has good decoupling performance and reveals great ability of attitude tracking as well as disturbance restraint.


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    Titel :

    Comprehensive nonlinear modeling and attitude control of a novel tandem ducted fan vehicle


    Beteiligte:
    Zhang, Yibo (Autor:in) / Xiang, Changle (Autor:in) / Xu, Bin (Autor:in) / Wang, Xiaoliang (Autor:in) / Fan, Wei (Autor:in)


    Erscheinungsdatum :

    01.10.2016


    Format / Umfang :

    437581 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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