This paper studies the problem of robust output tracking control for the homing phase of autonomous spacecraft rendezvous. Based on the C-W equations, parameter uncertainty and the output tracking requirement, a new relative dynamic model is developed, and a robust guaranteed cost output tracking control problem is formulated. Then, by a Lyapunov approach, the controller design is cast into a convex optimization problem subject to linear matrix inequalities (LMIs) constraints. With the obtained controllers, the homing phase can be completed with a guaranteed cost, and the poles of the closed-loop system are located within a desire region. An illustrative example is provided to show the effectiveness of the proposed controller design method.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Output tracking control for autonomous spacecraft rendezvous


    Contributors:
    Yang, Xuebo (author) / Bo, Yuming (author) / Liu, Yurong (author) / Ji, Zhijian (author) / Gao, Huijun (author)


    Publication date :

    2009


    Size :

    6 Seiten, 15 Quellen




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English