The effects of Sun attraction and solar radiation pressure on Medium Earth orbit Satellites
Abstract
The effects of the sun perturbations ( solar radiation pressure and the attraction of the sun ) at medium Earth orbit satellite and relation of solar radiation pressure have been investigated . Computer simulation of the equation of motion and velocity with perturbations is designed by matlab a 7.10 where using Jacobian matrix method to increase the accuracy .Downloads
Downloads
Published
How to Cite
Issue
Section
License
Copyright (c) 2012 Abbas Fadil Alrofiae, Suha Hadi Kadhem, Aref Saleh baron
This work is licensed under a Creative Commons Attribution 4.0 International License.
Journal of Kufa-Physics is licensed under the Creative Commons Attribution 4.0 International License, which allows users to copy, to create extracts, abstracts, and new works from the Article, to alter and revise the Article, and to make commercial use of the Article (including reuse and/or resale of the Article by commercial entities), provided the user gives appropriate credit (with a link to the formal publication through the relevant DOI), provides a link to the license, indicates if changes were made and the licensor is not represented as endorsing the use made of the work. The authors hold the copyright for their published work on the JKP website, while KJP is responsible for appreciating citation for their work, which is released under CC-BY-4.0 enabling the unrestricted use, distribution, and reproduction of an article in any medium, provided that the original work is properly cited.
