Abstract The problems of synthesis of attitude determination and control system of small satellites regarding the influence of external perturbations due to their small mass and restrictions in using high-precision actuators, due to the limitations of energy budget and construction, are considered. The solutions to this problem are proposed involving the development of high-accuracy algorithms for satellite attitude determination and control, using the minimum set of sensors, various types of actuators, and optimization principles.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Optimization Issues in the Problem of Small Satellite Attitude Determination and Control


    Beteiligte:
    Rakisheva, Zaure (Autor:in) / Sukhenko, Anna (Autor:in) / Kaliyeva, Nazgul (Autor:in)


    Erscheinungsdatum :

    2019-01-01


    Format / Umfang :

    21 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Onboard Attitude Determination for a Small Satellite

    Bak, T. | British Library Online Contents | 1997


    Comparison of small satellite attitude determination methods

    Marques, Sonia / Clements, Roberts / Lima, Pedro | AIAA | 2000


    Attitude Determination and Control System for a Small LEO Satellite

    Jan, Y.-W. / Ting, L. H. / COSPAR et al. | British Library Conference Proceedings | 1999



    Satellite attitude determination and control system

    MENG ZIYANG / SUN XIAOLONG / ZHANG GAOFEI | Europäisches Patentamt | 2020

    Freier Zugriff