As various types of perturbations tend to drive a geostationary satellite away from its prescribed position, occasional orbit corrections have to be carried out by means of a suitable propulsion system. In future geostationary missions, low thrust electric propulsion is likely to be applied for station keeping because of considerable mass savings. In this paper a station keeping strategy for electric propulsion systems is developed. Both the unconstrained case and the case where thrust operation constraints are present are considered and tested by computer simulation of a realistic example.
Station Keeping of Geostationary Satellites by Electric Propulsion
1985
43 pages
Report
Keine Angabe
Englisch
Unmanned Spacecraft , Electric & Ion Propulsion , Electric propulsion , Low thrust propulsion , Spacecraft control , Stationkeeping , Synchronous satellites , Computerized simulation , Earth orbits , Geosynchronous orbits , Orbital mechanics , Trajectory optimization , Foreign technology , Translations
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