Observational Arc-Length Effect on Orbit Determination for KPLO
In this study, orbit determination (OD) simulation for the Korea Pathfinder Lunar Orbiter (KPLO) was accomplished for investigation of the observational arc-length effect using a sequential estimation algorithm. A lunar polar orbit located at 100 km altitude and 90° inclination was mainly consider...
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| Hlavní autoři: | , , , |
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| Médium: | Artigo |
| Jazyk: | Inglês |
| Vydáno: |
The Korean Space Science Society
2018-12-01
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| Edice: | Journal of Astronomy and Space Sciences |
| Témata: | |
| On-line přístup: | http://janss.kr/journal/article.php?code=64506 |
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