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On the roto-translatory motion of a satellite of an oblate primary

✍ Scribed by J. M. Ferrándiz; M. E. Sansaturio; R. Caballero


Publisher
Springer Netherlands
Year
1993
Tongue
English
Weight
683 KB
Volume
57
Category
Article
ISSN
1572-9478

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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