The feasibility of achieving complex underactuated control based on a single orbital thruster with two inputs and six outputs is explored in this article. The study applies this control method to the attitude–orbit coupling control of the microsatellite during high-thrust orbital maneuver. An underactuated controller is introduced in the presence of partial states without direct inputs and multiple states actuated by single input. First, based on the orbit and attitude model, the input and underactuated characteristics are analyzed. Then, combining backstepping and hierarchical structure, an integral terminal sliding mode controller is designed to address the complex underactuation, while approximating the uncertainties using an adaptive fuzzy observer. Simulation results are presented to verify the underactuated attitude–orbit control performance of the proposed controller, thereby offering a crucial guarantee for the rapid maneuverability of microsatellite.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Underactuated Attitude–Orbit Coupling Control for Microsatellite Based on a Single Orbital Thruster


    Beteiligte:
    Lu, Junjie (Autor:in) / Meng, Zhongjie (Autor:in)


    Erscheinungsdatum :

    01.04.2024


    Format / Umfang :

    4108646 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Attitude and orbit control micro-thruster

    FENG FENG / GUO HONGJING / SHEN XIAODONG et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Space orbit attitude control water thruster

    FENG SONGJIANG / LIN WEI / HUO-YUAN TONGXIN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Design of Solar Thermal Thruster for Microsatellite Orbital Control

    Soliman, Maged A. / El Hadidi, Basman M. | AIAA | 2014



    Attitude and orbit integrated control method based on orbit control thruster pulse width modulation

    WU FAN / WANG FENG / CAO XIBIN et al. | Europäisches Patentamt | 2020

    Freier Zugriff