NASA NTRS · 19680004620
Guidance, flight mechanics and trajectory optimization. Volume 3 - The two-body problem
Abstract
Two body problem for satellite guidance, flight mechanics, and trajectory optimization analyses
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Tamburro, M. B., Townsend, G. E.. 1968-01-01. Guidance, flight mechanics and trajectory optimization. Volume 3 - The two-body problem. https://ntrs.nasa.gov/citations/19680004620
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