This chapter shows the equations used in the JPL computer program ASAP that are specific to the modeling of the central body disturbing function, the third-body disturbing function, as well as the equations of motion due to atmospheric drag. These descriptions are taken directly from Reference [1] by Kwok.
The Mathematical Models of the Jet Propulsion Laboratory (JPL) Artificial Satellite Analysis Program (ASAP)
Space Technology Library
13.04.2021
5 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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