Some useful results on initial node locations for near-equatorial circular satellite orbits-Reference-Cited by-同舟云学术

Some useful results on initial node locations for near-equatorial circular satellite orbits

Published:1973-08 Issue:1 Volume:8 Page:45-73
ISSN:0008-8714
Container-title:Celestial Mechanics
language:en
Short-container-title:Celestial Mechanics

Author:

Kamel Ahmed,Tibbitts Richard

Publisher

Springer Science and Business Media LLC

Subject

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

Link

http://link.springer.com/content/pdf/10.1007/BF01228389.pdf

Reference13 articles.

1. Allan, R. R.: 1963, Lunisolar Effects, Royal Aircraft Establishment, Technical Note Space 47.

2. Billik, B. H.: 1967,J. Spacecraft 4, No. 3.

3. Bryson, A. E. and Ho, Y.: 1969,Applied Optimal Contral, Blaisdell Publishing Company.

4. Deprit, A.: 1969,Celes. Mech. 1, 12.

5. Deutsch, R.: 1963,Orbital Dynamics of Space Vehicles, Prentice-Hall Inc., Englewood Cliffs, N.J.

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