The nonlinear backstepping adaptive controller is designed for the large angle fast attitude maneuver of spacecraft with uncertainties in the moment of inertia. Deviation between the actual position and command position is depicted by error quaternion. The nonlinear backstepping tracking function is employed to design the adaptive controller both of command torque and estimation of unknown moment inertia. And the stability is analyzed based on Lyapunovo function. By Matlab/Simulink programming, the simulation of spacecraft attitude manoeuver control is discussed, and its results demonstrate the effectiveness and feasibility of the proposed controller.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Nonlinear Back Stepping Adaptive Controller Design for Spacecraft Attitude Maneuver



    Erschienen in:

    Erscheinungsdatum :

    2014-07-18


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Vibration Control of Flexible Spacecraft Under Attitude Maneuver Using Adaptive Controller

    Oh, Choongseok / Bang, Hyochoong / Park, Jong-Oh | AIAA | 2006


    AIAA-2006-6182 Vibration Control of Flexible Spacecraft Under Attitude Maneuver Using Adaptive Controller

    Oh, C. / Bang, H. / Park, J. et al. | British Library Conference Proceedings | 2006


    Genetic Algorithm-Aided Fuzzy Controller for Spacecraft Attitude Maneuver with Uncertainties

    Choi, Daegyun / Chhabra, Anirudh / Kim, Donghoon | AIAA | 2021


    Guidance Templates for Spacecraft Attitude Maneuver Planning

    Miller, Andrew J. / Akella, Maruthi R. | AIAA | 2024


    Spacecraft Attitude Controller Design for Large Angle Maneuver Using Quaternion and Dual Mode Control

    Nam, H. S. / Kim, S. H. / Song, C. H. et al. | British Library Conference Proceedings | 1999