AIR DRAG CORRECTION FOR SATELLITE ORBITS OF LOW ECCENTRICITY

被引：1
|
作者：
BROOKES, CJ
机构：
来源：
PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES | 1992年 / 437卷 / 1899期
关键词：
D O I：
10.1098/rspa.1992.0054
中图分类号：
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号：
07 ; 0710 ; 09 ;
摘要：
A method is derived for removing the perturbations in eccentricity due to the effects of air drag, on satellite orbits of low eccentricity and, in particular, for those lying in planes inclined at angles close to the critical angle of inclination of 63.4-degrees, for which the oscillation in eccentricity due to the Earth's gravity field is significantly large.
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页码：175 / 183
页数：9
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