Orbital Evolution of Space Debris
In order to obtain a complete picture of the time dependent dynamic of 360 fragment in space, the program IODS(ISSA Orbit Determination System) has been set up. Using The program IODS, all fragments orbit of one break-up event can be generated. Perturbation due to the Earth's asymmetrical poten...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
The Korean Space Science Society
1991-12-01
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| Series: | Journal of Astronomy and Space Sciences |
| Online Access: | http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1991/v8n2/OJOOBS_1991_v8n2_141.pdf |
| Summary: | In order to obtain a complete picture of the time dependent dynamic of 360 fragment in space, the program IODS(ISSA Orbit Determination System) has been set up. Using The program IODS, all fragments orbit of one break-up event can be generated. Perturbation due to the Earth's asymmetrical potential, the Sun, moon, air drag, and solar radiation force are considered. We summarize our results as follows; Due to J2 term, precessional motion of all fragment orbits are 0.5 day < d/dt < 1.4/day) The other perturbations have very small effect. |
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| ISSN: | 2093-5587 2093-1409 |