We consider a small information satellite which may be placed on an orbit with altitude from 600 up to 1000 km. The satellite attitude and orbit control system contains a strap-down inertial navigation system, cluster of four reaction wheels, magnetic driver and a correcting engine unit with eight electro-reaction engines. We study problems on design of algorithms for spatial guidance, in-flight identification and adaptive-robust control of the satellite motion on sun-synchronous orbit.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Guidance and adaptive-robust attitude & orbit control of a small information satellite


    Beteiligte:
    Somov, Ye. (Autor:in) / Butyrin, S. (Autor:in) / Somov, S. (Autor:in) / Somova, T. (Autor:in) / Testoyedov, N. (Autor:in) / Rayevsky, V. (Autor:in) / Titov, G. (Autor:in) / Yakimov, Ye. (Autor:in) / Ovchinnikov, A. (Autor:in) / Mathylenko, M. (Autor:in)

    Kongress:

    ICNPAA 2016 WORLD CONGRESS: 11th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences ; 2016 ; La Rochelle, France


    Erschienen in:

    Erscheinungsdatum :

    27.01.2017


    Format / Umfang :

    10 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Robust attitude control for flexible satellite during orbit maneuver

    Li, Long / Yang, Jing / Shi, Xiaoping et al. | IEEE | 2014


    Robust control for satellite attitude regulation during on-orbit assembly

    Lingling Shi / Kinkaid, Nathan / Katupitiya, Jayantha | IEEE | 2016


    Drag-based propellant-less small satellite attitude orbit and de-orbit control system

    BEVILACQUA RICCARDO / GUGLIELMO DAVID C / OMAR SANNY et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    DRAG-BASED PROPELLANT-LESS SMALL SATELLITE ATTITUDE ORBIT AND DE-ORBIT CONTROL SYSTEM

    BEVILACQUA RICCARDO / GUGLIELMO DAVID C / OMAR SANNY et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    DRAG-BASED PROPELLANT-LESS SMALL SATELLITE ATTITUDE ORBIT AND DE-ORBIT CONTROL SYSTEM

    BEVILACQUA RICCARDO / GUGLIELMO DAVID C / OMAR SANNY et al. | Europäisches Patentamt | 2020

    Freier Zugriff