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.
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
1976
36 pages
Report
No indication
English
Optimal Geostationary Satellite Collocation Using Relative Orbital Element Corrections
Online Contents | 2009
|Optimal Geostationary Satellite Collocation Using Relative Orbital Element Corrections
British Library Conference Proceedings | 2009
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