The main problem of artificial satellite theory for small and moderate eccentricities
- 1 June 1970
- journal article
- research article
- Published by Springer Nature in Celestial Mechanics and Dynamical Astronomy
- Vol. 2 (2) , 166-206
- https://doi.org/10.1007/bf01229494
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Canonical transformations depending on a small parameterCelestial Mechanics and Dynamical Astronomy, 1969
- Numerical integration of an orbit and its concomitant variations by recurrent power seriesZeitschrift für angewandte Mathematik und Physik, 1966
- Telstar orbit prediction method - Accuracy comparison with other orbit prediction methods.AIAA Journal, 1966
- Determination of mean elements for Brouwer's satellite theoryThe Astronomical Journal, 1962
- Solution of the problem of artificial satellite theory without dragThe Astronomical Journal, 1959