This article addresses the problem of spacecraft reorientation subject to attitude pointing, angular velocity, and actuator constraints. In order to tackle the attitude pointing constraints, a potential function is proposed, which is parameterized to allow for a wider range of optimal repointing solutions with attitude pointing constraints. Based on the potential function, a feedback control law is then designed for ensuring the system stability. The controller gains are optimized using a gradient-based optimal parameter tuning method. Furthermore, by imposing the angular velocity constraints and the actuator constraints into the formulation, the optimal parameter tuning method also ensures the satisfaction of these constraints. Therefore, stability, optimality, and feasibility are achieved simultaneously. Numerical simulations demonstrate accurate repointing maneuvering under different types of constraints.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Constrained Feedback Control for Spacecraft Reorientation With an Optimal Gain


    Beteiligte:
    Li, Bin (Autor:in) / Wang, Yang (Autor:in) / Zhang, Kai (Autor:in) / Duan, Guang-Ren (Autor:in)


    Erscheinungsdatum :

    01.12.2021


    Format / Umfang :

    1767992 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    An Optimal Feedback Control Law for Spacecraft Reorientation with Attitude Pointing Constraints

    Li, Bin / Wang, Yang / Zhang, Kai | British Library Conference Proceedings | 2021


    Comments on the Convex Constrained Spacecraft Reorientation

    Mashtakov, Yaroslav / Shestakov, Sergey | IEEE | 2023


    Optimal Reorientation Of Spacecraft Orbit

    Chelnokov, Yuriy Nikolaevich / Pankratov, Ilya Alekseevich / Sapunkov, Yakov Grigorievich | Tema Archiv | 2014