A development of an analytical solution for the motion of an artificial Earth satellite subject to the combined effects of Earth gravity and air drag is presented. The atmospheric model takes into account a linear variation of the density scale height with altitude, the rotation and the oblateness o
โฆ LIBER โฆ
Trajectories of satellites under the combined influences of earth oblateness and air drag
โ Scribed by Chong-Hung Zee
- Publisher
- Springer Netherlands
- Year
- 1971
- Tongue
- English
- Weight
- 796 KB
- Volume
- 3
- Category
- Article
- ISSN
- 1572-9478
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