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Design of trajectory and perturbation analysis for satellite orbital parameters
M. Raja, Saurabh Pandey, Rishabh Kumar and Aman Dalmia

Published in: Journal for Advance Research in Applied Sciences
Volume- 4, Issue-4, pp.7-17, Sep 2017
DPI :-> 16.10089.JARAS.2017.V4I4.717.1936



Abstract
The aviation and space industry is advancing at a fast pace. In light of the launch and re-entry accidents that have happened in the past it is essential to have accurate analysis of the parameters required for error free launch and placement of the launched body in correct trajectory. In this paper we discuss various orbital parameters required for placing a satellite, launched from earth, in correct orbit and the designing of its trajectory using Patched Conic Approximation method. Also presented are various perturbations factors like lunar gravity and atmospheric drag. The effect of these factors is considered and compared with the ideal cases.

Key-Words / Index Term
Keplerian elements, perturbation, patched conic approximation method, atmospheric drag.

How to cite this article
M. Raja, Saurabh Pandey, Rishabh Kumar and Aman Dalmia , “Design of trajectory and perturbation analysis for satellite orbital parameters”, Journal for Advance Research in Applied Sciences, 4, Issue-4, pp.7-17, Sep 2017. DPI:16.10089.JARAS.V4.I4.1936