Close-proximity tracking control of a rotating space object is investigated in this paper. The control objectives are relative position and attitude tracking and keeping, which include keeping the spacecraft stay at a certain distance above the specific face of the object, and keeping the spacecraft’s certain body-fixed axis pointing to the object during the process. This problem is challenging because the desired motion of the tracking spacecraft is determined by both the object’s attitude status and the relative motion between the spacecraft and the object. A nonlinear orbit-attitude coordinated adaptive tracking controller is developed to fulfill the tracking mission. The sufficient condition for the asymptotic stability is investigated. The influences of the uncertainties including the mass and inertial matrix of the spacecraft and disturbance are taken into consideration. Numerical simulations demonstrate the effectiveness of the tracking control.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rotating Object Specific Tracking Based on Orbit-Attitude Coordinated Adaptive Control


    Beteiligte:
    Zhu, Lingchao (Autor:in) / Wang, Shuquan (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.02.2021




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    ADAPTIVE AUGMENTING CONTROL OF SATELLITE ATTITUDE FOR OBJECT TRACKING FROM RELATIVE ORBIT

    Franquiz, Francisco J. / Sanchez, Luis A. / Udrea, Bogdan et al. | British Library Conference Proceedings | 2016


    Adaptive Augmenting Control of Satellite Attitude for Object Tracking from Relative Orbit

    Franquiz, Francisco J. / Udrea, Bogdan / Sanchez, Luis A. et al. | AIAA | 2016




    Orbit attitude control device, and method of controlling orbit attitude

    FUJITA TOSHIHARU / HAYAKAWA NOBUAKI | Europäisches Patentamt | 2016

    Freier Zugriff