Abstract The system of spacecraft angular stabilization of middle accuracy rating and with magnetic executive devices is considered. A three-axis magnetometer is used as a single sensitive element of the subsystem of attitude determination. Combination of specific features of the control law and the algorithm of attitude determination allows one to realize a sufficiently reliable stabilization system of simple design, which is rather economical, as far as computing time is concerned.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Magnetic stabilization of a spacecraft and the effect of compensation of information errors


    Beteiligte:

    Erschienen in:

    Cosmic Research ; 50 , 1 ; 76-85


    Erscheinungsdatum :

    2012-02-01


    Format / Umfang :

    10 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    SPACECRAFT STABILIZATION SYSTEM

    ASJUSHKIN VLADIMIR ANDREEVICH / DISHEL VALERIJ DAVIDOVICH / ISHIN SERGEJ VJACHESLAVOVICH et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    Magnetic spacecraft attitude stabilization with two torquers

    Alger, Mike / de Ruiter, Anton | Elsevier | 2021


    Spacecraft stabilization system

    Online Contents | 1995