This paper investigates the problem of distributed attitude control for spacecraft formation flying systems based on the Takagi- Sugeno (T-S) fuzzy modeling method, where external disturbances and parameter uncertainties are considered. The spacecraft attitude dynamics is constructed as T-S fuzzy model anda modified distributed fuzzy-based H controller is designed. It is proven that the attitude of multispacecraft can synchronously reach zero by using the designed controller. Numerical examples are provided to illustrate the effectiveness of the proposed controller and comparisons with the existing results.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Distributed Attitude Control for Multispacecraft via Takagi–Sugeno Fuzzy Approach


    Contributors:
    Zhuo Zhang (author) / Zexu Zhang (author) / Hui Zhang (author)


    Publication date :

    2018-04-01


    Size :

    1373501 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    An Approach for Building Takagi-Sugeno Fuzzy Models

    Liu, X.-c. / Liang, Y. / Pan, Q. et al. | British Library Online Contents | 2006




    Resilient Attitude Alignment in Multispacecraft Systems

    Rezaee, Hamed / Abdollahi, Farzaneh | IEEE | 2019