Air drag effect on the motion of an arti
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Y. M. Almleakyd; Y. E. Helali; H. M. Basurah; A. A. Malawi; A. A. Goharji; M. N.
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Article
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1996
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Springer Netherlands
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English
β 332 KB
Two methods have been used to compute and compare the perturbations in perigee distance for an artificial Earth satellite. The two methods have used different air density models. The first (Helali, 1987) used the TD model, formulated by Sehnel(1986a), which contains terms that describe all the princ