Orbital Elements Evolution Due to a Perturbing Body in an Inclined Elliptical Orbit
This paper intends to highlight the effect of the third-body in an inclined orbit on a spacecraft orbiting the primary mass. To achieve this goal, a new origin of coordinate is introduced in the primary and the X-axis toward the node of the spacecraft. The disturbing function is expanded up to the s...
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| Format: | Article |
| Language: | English |
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Korean Space Science Society (KSSS)
2014-09-01
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| Series: | Journal of Astronomy and Space Sciences |
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| Online Access: | http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2014/v31n3/OJOOBS_2014_v31n3_199.pdf |