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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: Razali, Radzuan, Kamal Adnan, Muhammad Shamsul
Format: Citation Index Journal
Published: Centre for promoting ideas, USA 2011
Subjects:
QA76 Computer software
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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spelling my.utp.eprints.56552017-01-19T08:22:52Z Mathematical Modeling and software development on pertubation effects towards small satellite mission on low earth orbit (LEO) Razali, Radzuan Kamal Adnan, Muhammad Shamsul QA76 Computer software 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 perturbation of low altitude orbits due to the oblate shape of the earth. This gravitational effect of an oblate earth can be modeled by using Spherical Harmonics to satisfy the Laplace’s Equation. A precise calculation of the perturbations is possible only if the orbit is sufficiently well known. The results can be obtained by using Ordinary Differential Equation, i.e., Runge-Kutta method, and Matlab to view the graphs. This paper discusses the development of Mathematical Modeling and Analysis Software on Perturbation Effects Using Cowell’s Method and with the help of Matlab to visualize the Effect. Centre for promoting ideas, USA 2011-03-31 Citation Index Journal PeerReviewed application/pdf http://eprints.utp.edu.my/5655/1/Paper_1.pdf http://www.ijast.com Razali, Radzuan and Kamal Adnan, Muhammad Shamsul (2011) Mathematical Modeling and software development on pertubation effects towards small satellite mission on low earth orbit (LEO). [Citation Index Journal] http://eprints.utp.edu.my/5655/
institution Universiti Teknologi Petronas
building UTP Resource Centre
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Petronas
content_source UTP Institutional Repository
url_provider http://eprints.utp.edu.my/
topic QA76 Computer software
spellingShingle QA76 Computer software
Razali, Radzuan
Kamal Adnan, Muhammad Shamsul
Mathematical Modeling and software development on pertubation effects towards small satellite mission on low earth orbit (LEO)
description 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 perturbation of low altitude orbits due to the oblate shape of the earth. This gravitational effect of an oblate earth can be modeled by using Spherical Harmonics to satisfy the Laplace’s Equation. A precise calculation of the perturbations is possible only if the orbit is sufficiently well known. The results can be obtained by using Ordinary Differential Equation, i.e., Runge-Kutta method, and Matlab to view the graphs. This paper discusses the development of Mathematical Modeling and Analysis Software on Perturbation Effects Using Cowell’s Method and with the help of Matlab to visualize the Effect.
format Citation Index Journal
author Razali, Radzuan
Kamal Adnan, Muhammad Shamsul
author_facet Razali, Radzuan
Kamal Adnan, Muhammad Shamsul
author_sort Razali, Radzuan
title Mathematical Modeling and software development on pertubation effects towards small satellite mission on low earth orbit (LEO)
title_short Mathematical Modeling and software development on pertubation effects towards small satellite mission on low earth orbit (LEO)
title_full Mathematical Modeling and software development on pertubation effects towards small satellite mission on low earth orbit (LEO)
title_fullStr Mathematical Modeling and software development on pertubation effects towards small satellite mission on low earth orbit (LEO)
title_full_unstemmed Mathematical Modeling and software development on pertubation effects towards small satellite mission on low earth orbit (LEO)
title_sort mathematical modeling and software development on pertubation effects towards small satellite mission on low earth orbit (leo)
publisher Centre for promoting ideas, USA
publishDate 2011
url http://eprints.utp.edu.my/5655/1/Paper_1.pdf
http://www.ijast.com
http://eprints.utp.edu.my/5655/
_version_ 1738655420143108096
score 13.211869

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