| Autor: |
Amin, Mohamed R. |
| Předmět: |
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| Zdroj: |
Mechanics & Mechanical Engineering; 2020, Vol. 24 Issue 1, p56-60, 5p |
| Abstrakt: |
The focus of this paper is the design of a self-maintenance orbit using two natural forces against each other. The effect of perturbations due to Earth’s oblateness up to the third order on both the semi-major axis and eccentricity for a low Earth orbit satellite together with the perturbation due to air drag on the same orbital parameters were used, in order to create self-maintenance orbits. Numerical results were simulated for a low earth orbit satellite, which substantiates the applicability of the results. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Complementary Index |
| Externí odkaz: |
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