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Relative motion of orbiting bodies
Author(s) -
Eugene I. Butikov
Publication year - 2001
Publication title -
american journal of physics
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.541
H-Index - 99
eISSN - 1943-2909
pISSN - 0002-9505
DOI - 10.1119/1.1313520
Subject(s) - physics , relative motion , motion (physics) , orbit (dynamics) , orbital motion , classical mechanics , orbital elements , orbital mechanics , circular orbit , differential (mechanical device) , mean motion , celestial mechanics , aerospace engineering , astronomy , planet , angular momentum , satellite , engineering , thermodynamics
A problem of relative motion of orbiting bodies is investigated on the example of the free motion of any body ejected from the orbital station that stays in a circular orbit around the earth. An elementary approach is illustrated by a simulation computer program and supported by a mathematical treatment based on approximate dierential equations of the relative orbital motion. 1. Relative motion of bodies in space orbits—an introductory approach

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