Long-term evolution of Galileo operational orbits by canonical perturbation theory

被引:10
|
作者
Lara, Martin
San-Juan, Juan F. [1 ]
Lopez-Ochoa, Luis M. [1 ]
Cefola, Paul [2 ]
机构
[1] Univ La Rioja, Logrono, Spain
[2] SUNY Buffalo, Amherst, NY USA
关键词
Galileo orbits; Tesseral resonances; Averaging; Intermediaries; Semi-analytical satellite theory; RESONANT LUNISOLAR PERTURBATIONS; EARTH SATELLITE ORBITS; DYNAMICAL EVOLUTION; ECCENTRICITY;
D O I
10.1016/j.actaastro.2013.09.008
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Galileo operational orbits are slightly affected by the 3 to 5 tesseral resonance, an effect that can be much more important in the case of disposal orbits. Proceeding by canonical perturbation theory we show that the part of the long-term Hamiltonian corresponding to the non-centralities of the Earth's gravitational potential can be replaced by an intermediary that shows the pendulum dynamics of the 3 to 5 tesseral resonance problem. Inclusion of lunisolar perturbations requires a semi-analytical integration, which is compared with the corresponding results from the well-established Draper Semi-analytical Satellite Theory. (C) 2013 IAA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:646 / 655
页数:10
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