The effect of attitude corrections for geostationary satellite stationkeeping by means of ion thrustors was investigated. It is essential to control perturbations induced in the orbital plane. These perturbations will closely depend on the attitude guidance mode during thrust. A model was set up for the evolution of the orbital plane, as well as a model for the in-plane perturbing effect. Three different hypotheses were chosen for the attitude guidance mode. The effect of the corrections on the in-plane orbital elements for each one is described. The results should be useful for feasibility studies of inclination corrections by ion thrustors.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Orbital Conditions of a Geosynchronous Satellite: Effects Induced in the Orbital Plane by North-South Corrections Corrections d'Orbites d'UN Satellite Geosynchrone: Etude des Effets Induits dans le Plan de l'Orbite Par des Corrections Nord-Sud


    Beteiligte:
    A. Esterle (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    36 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Optimal Geostationary Satellite Collocation Using Relative Orbital Element Corrections

    Beigelman, I. / Gurfil, P. / European Space Agency | British Library Conference Proceedings | 2009



    SYSTÈME ET MÉTHODE D'ANALYSE D'ORBITES MONO-SATELLITE

    HENNART FLORENT | Europäisches Patentamt | 2021

    Freier Zugriff

    SYSTÈME ET MÉTHODE D'ANALYSE D'ORBITES MONO-SATELLITE

    HENNART FLORENT | Europäisches Patentamt | 2023

    Freier Zugriff