Third-Order Solution to the Main Problem in Satellite Theory
Author:
Affiliation:
1. Naval Research Laboratory, Washington, D.C.
2. National Bureau of Standards, Washington, D.C.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.56183
Reference14 articles.
1. The main problem of artificial satellite theory for small and moderate eccentricities
2. Analytical theory of earth's artificial satellites (A.T.E.A.S.)
3. 3Kinoshita, H. "Third-Order Solution of an Artificial Satellite Theory," Smithsonian Astrophysical Observatory, Kept. 379,1977.
4. Solution of the problem of artificial satellite theory without drag
5. Second-order solution of artificial satellite theory without air drag
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