The main problem of artificial satellite theory for small and moderate eccentricities-Reference-Cited by-同舟云学术

The main problem of artificial satellite theory for small and moderate eccentricities

Published:1970-06 Issue:2 Volume:2 Page:166-206
ISSN:0008-8714
Container-title:Celestial Mechanics
language:en
Short-container-title:Celestial Mechanics

Author:

Deprit Andr�,Rom Arnold

Publisher

Springer Science and Business Media LLC

Subject

General Medicine,Space and Planetary Science,Astronomy and Astrophysics,Applied Mathematics,Computational Mathematics,Mathematical Physics,Modeling and Simulation

Link

http://link.springer.com/content/pdf/10.1007/BF01229494.pdf

Reference16 articles.

1. Aksnes, K.: 1967,Astroph. Norv. 10, 156.

2. Arsenault, J. L., Enright, J. D., and Purcell, C.: 1964, ASTIA Documents 437-75 and 437-76.

3. Bonavito, N. L., Watson, S., and Walden, H.: 1969, NASA TN D-5203.

4. Brouwer, D.: 1959,Astron. J. 64, 378.

5. Brouwer, D. and Clemence, G. M.: 1961,Methods of Celestial Mechanics, Academic Press, New York, Ch.II, p. 79.

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