Dynamics of Satellites with Multi-Day Periods
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Publisher
Springer Netherlands
Link
http://link.springer.com/content/pdf/10.1007/978-94-015-9221-5_29
Reference10 articles.
1. Cook, G. E. (1972) Basic theory for PROD, a program for computing the development of satellite orbits, Celestial Mechanics 7, 301–314.
2. Roth, E. A. (1973) Fast computation of high eccentricity orbits by the stroboscopic method, Celestial Mechanics 8, 245–249.
3. Giacaglia, G. E. O. (1974) Lunar perturbations of artificial satellites of the Earth, Celestial Mechanics 9, 239–267.
4. Janin, G. (1974) Accurate computation of highly eccentric satellite orbits, Celestial Mechanics 10, 451–467.
5. Lane. M. T. (1989) On analytic modeling of lunar perturbations of artificial satellites of the Earth, Celestial Mechanics 46, 287–305.
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