A distributed attitude coordination control scheme using terminal sliding mode (TSM) is proposed for a group of spacecraft in the presence of external disturbances. A novel fast terminal sliding manifold is presented, and a robust control term based on the hyperbolic tangent function is employed to suppress bounded external disturbances. The finite-time stability of the overall closed-loop system is guaranteed by a Lyapunov-based approach, and numerical simulations are presented to demonstrate the performance of the proposed controller.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Distributed Attitude Coordination Control for Spacecraft Formation Flying


    Contributors:
    An-Min Zou, (author) / Kumar, K. D. (author)


    Publication date :

    2012-04-01


    Size :

    5103202 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English