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ANALYSIS OF THE MOTION OF A TETHER-PERTURBED SATELLITE
Author(s) -
Sung-Ki Cho,
Jae-Hoon Kim
Publication year - 2003
Publication title -
journal of astronomy and space sciences
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.273
H-Index - 11
eISSN - 2093-5587
pISSN - 2093-1409
DOI - 10.5140/jass.2003.20.4.319
Subject(s) - perturbation (astronomy) , physics , satellite , libration (molecule) , gravitational field , classical mechanics , geodesy , center of mass (relativistic) , gravitation , motion (physics) , geology , astronomy , geometry , mathematics , point (geometry) , energy–momentum relation
The motion of each satellite in a tethered satellite system is non-Keplerian in the Earth's gravitational field. In this paper, the tether perturbation force is formulated and compared with the perturbation force due to the Earth's oblateness. Also, the center of mass motion of the tethered satellite system is analyzed. The tether perturbing force on the one of satellites in a tethered satellite system is much bigger than the Earth's oblateness perturbation. The two-body motion approximation of the center of mass is acceptable to describe the motion of the system, when the libration is small

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