Mathematical Modeling and software development on pertubation effects towards small satellite mission on low earth orbit (LEO)
The orbit of satellite cannot be calculated using the theoretical method for precise calculation. This is because the orbital elements will deviate from true elements with time. Regression of the lines-of-the-nodes and rotation of the line-of-apsides (major axis) are the two principal effect of the...
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| 主要な著者: | , |
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| フォーマット: | Citation Index Journal |
| 出版事項: |
Centre for promoting ideas, USA
2011
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| オンライン･アクセス: | http://eprints.utp.edu.my/5655/1/Paper_1.pdf http://www.ijast.com http://eprints.utp.edu.my/5655/ |
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