This paper studies optimal sliding mode controller designs using integral sliding mode control (ISM) to deal with some spacecraft attitude control problems. Integral sliding mode control combining the first order sliding mode and optimal control is applied to quaternion-based attitude control for rest-to-rest manoeuvres with external disturbances. For the optimal control part, the state dependent Riccati equation (SDRE) approach and control Lyapunov function (CLF) are used to solve the infinite-time nonlinear optimal problem. The second method of Lyapunov is used to show that asymptotic stability is achieved. An example of rest-to-rest attitude manoeuvres is presented and simulation results are included to verify and compare the usefulness of the various controllers.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Optimal sliding mode controllers for spacecraft attitude manoeuvres


    Additional title:

    Optimale Sliding-Mode-Regler für Raumschiff-Orientierungsmanöver


    Contributors:


    Publication date :

    2009


    Size :

    6 Seiten, 11 Bilder, 19 Quellen


    Type of media :

    Conference paper


    Type of material :

    Storage medium


    Language :

    English




    Minimum Time & Fuel & Sliding Mode Controllers for Spacecraft Attitude Control

    Titus, H. / Cooper, C. R. / AIAA | British Library Conference Proceedings | 1994


    Attitude Manoeuvres

    Tewari, Ashish | Wiley | 2021


    Quasi-continuous higher order sliding-mode controllers for spacecraft-attitude-tracking maneuvers

    Pukdeboon, Chutiphon / Zinober, Alan S.I. / Thein, May-Win L. | Tema Archive | 2010



    Optimal Trajectory Attitude Manoeuvres for Lunar Missions

    Ercoli Finzi, A. / Vasile, M. / International Astronomical Federation | British Library Conference Proceedings | 1998