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Published in 2017 at "Aircraft Engineering and Aerospace Technology"
DOI: 10.1108/aeat-03-2015-0092
Abstract: Purpose The purpose of this paper is to study the effect of J3 perturbation of the Earth’s oblateness on satellite orbit compared with J2 perturbation. Design/methodology/approach Based on the parametric variation method in the time…
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Keywords:
argument perigee;
effect perturbation;
effect;
satellite orbit ... See more keywords