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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Bibliographic Details
Main Authors: Razali, Radzuan, Kamal Adnan, Muhammad Shamsul
Format: Citation Index Journal
Published: Centre for promoting ideas, USA 2011
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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