ANALYTICAL LINEAR PERTURBATION-THEORY FOR HIGHLY ECCENTRIC SATELLITE ORBITS

Authors
BRUMBERG E BRUMBERG VA KONRAD T SOFFEL M
Citation
E. Brumberg et al., ANALYTICAL LINEAR PERTURBATION-THEORY FOR HIGHLY ECCENTRIC SATELLITE ORBITS, Celestial mechanics & dynamical astronomy, 61(4), 1995, pp. 369-387
Citations number
NO
Categorie Soggetti
Astronomy & Astrophysics
Journal title
Celestial mechanics & dynamical astronomy → ACNP
ISSN journal
09232958
Volume
61
Issue
4
Year of publication
1995
Pages
369 - 387
Database
ISI
SICI code
0923-2958(1995)61:4<369:ALPFHE>2.0.ZU;2-F
Abstract
Kaula's satellite linear perturbation theory has-been extended for the case of highly eccentric orbits by using elliptic function expansions .