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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| Main Authors: | , |
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| Format: | Citation Index Journal |
| Published: |
Centre for promoting ideas, USA
2011
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| Subjects: | |
| Online Access: | http://eprints.utp.edu.my/5655/1/Paper_1.pdf http://www.ijast.com http://eprints.utp.edu.my/5655/ |
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