Orbital perturbations and stationkeeping of communication satellites
- 1 March 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 15 (2) , 67-78
- https://doi.org/10.2514/3.27999
Abstract
No abstract availableKeywords
This publication has 39 references indexed in Scilit:
- Some useful results on initial node locations for near-equatorial circular satellite orbitsCelestial Mechanics and Dynamical Astronomy, 1973
- Zur Bahnberechnung von Geostationären SatellitenCelestial Mechanics and Dynamical Astronomy, 1973
- Analytical study of the Earth's shadowing effects on satellite orbitsCelestial Mechanics and Dynamical Astronomy, 1972
- Equilibrium longitudes of geostationary satellites.AIAA Journal, 1968
- Solar radiation pressure and the motion of earth satellitesAIAA Journal, 1963
- Perturbations of a geostationary satellite by the longitude-dependent terms in the earth's gravitational fieldPlanetary and Space Science, 1963
- ATTITUDE CONTROL AND STATION KEEPING OF A COMMUNICATION SATELLITE IN A 24-HOUR ORBITAIAA Journal, 1963
- FLIGHT MECHANICS OF THE 24-HOUR SATELLITEAIAA Journal, 1963
- The effect of solar radiation pressure on the motion of an artificial satelliteThe Astronomical Journal, 1961
- Effects of Solar Radiation Pressure on Earth Satellite OrbitsScience, 1960