NDLI: On the third-body perturbations of high-altitude orbits

Content Provider	Springer Nature Link
Author	Lara, Martin San Juan, Juan F. López, Luis M. Cefola, Paul J.
Copyright Year	2012
Abstract	The long-term effects of a distant third-body on a massless satellite that is orbiting an oblate body are studied for a high order expansion of the third-body disturbing function. This high order may be required, for instance, for Earth artificial satellites in the so-called MEO region. After filtering analytically the short-period angles via averaging, the evolution of the orbital elements is efficiently integrated numerically with very long step-sizes. The necessity of retaining higher orders in the expansion of the third-body disturbing function becomes apparent when recovering the short-periodic effects required in the computation of reliable osculating elements.
Starting Page	435
Ending Page	452
Page Count	18
File Format	PDF
ISSN	09232958
Journal	Celestial Mechanics and Dynamical Astronomy
Volume Number	113
Issue Number	4
e-ISSN	15729478
Language	English
Publisher	Springer Netherlands
Publisher Date	2012-07-25
Publisher Place	Dordrecht
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	Third-body perturbation Lie transforms Averaging High-altitude orbits Astrophysics and Astroparticles Mechanics Aerospace Technology and Astronautics Dynamical Systems and Ergodic Theory Geophysics/Geodesy
Content Type	Text
Resource Type	Article
Subject	Applied Mathematics Mathematical Physics Astronomy and Astrophysics Modeling and Simulation Computational Mathematics Space and Planetary Science

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