DERIVATION OF NODAL PERIOD OF AN EARTH SATELLITE AND COMPARISONS OF SEVERAL FIRST-ORDER SECULAR OBLATENESS RESULTS
Author:
Affiliation:
1. The Martin Company, Baltimore, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.1990
Reference29 articles.
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