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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    Title :

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


    Contributors:
    Zhang, Yibo (author) / Xiang, Changle (author) / Xu, Bin (author) / Wang, Xiaoliang (author) / Fan, Wei (author)


    Publication date :

    2016-10-01


    Size :

    437581 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





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