Analytical Third Order Solution for Coupling Effects of Earth Oblateness and Direct Solar Radiation Pressure on the Motion of Artificial Satellites  

Analytical Third Order Solution for Coupling Effects of Earth Oblateness and Direct Solar Radiation Pressure on the Motion of Artificial Satellites

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作  者:Hadia Hassan Selim 

机构地区:[1]Department of Astronomy, National Research Institute of Astronomy and Geophysics, Cairo, Egypt

出  处:《International Journal of Astronomy and Astrophysics》2014年第3期530-543,共14页天文学与天体物理学国际期刊(英文)

摘  要:Coupling effects of Earth oblateness and direct solar radiation pressure on the motion of an artificial satellite are evaluated. Secular and periodic terms are retained up to order three and two respectively, where the coefficient of the second zonal harmonic of the geopotential is considered of first order. The solution revealed the existence of secular terms at order three that arises from the couplings between terms, of lower orders, resulting from the solar radiation pressure.Coupling effects of Earth oblateness and direct solar radiation pressure on the motion of an artificial satellite are evaluated. Secular and periodic terms are retained up to order three and two respectively, where the coefficient of the second zonal harmonic of the geopotential is considered of first order. The solution revealed the existence of secular terms at order three that arises from the couplings between terms, of lower orders, resulting from the solar radiation pressure.

关 键 词:EARTH Oblateness-Solar Radiation Pressure-Artificial SATELLITES 

分 类 号:O1[理学—数学]

 

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