Modeling, dynamics and control of spacecraft relative motion in a perturbed keplerian orbit

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Modeling, dynamics and control of spacecraft relative motion in a perturbed keplerian orbit

The dynamics of relative motion in a perturbed orbital environment are exploited based on Gauss’ and Cowell’s variational equations. The inertial coordinate frame and relative coordinate frame (Hill frame) are used, and a linear high fidelity model is developed to describe the relative motion. This...

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Bibliographic Details
Main Authors:	Okasha, Mohamed Elsayed Aly Abd Elaziz, Newman, Brett
Format:	Article
Language:	English English
Published:	The Korean Society for Aeronautical & Space Sciences 2015
Subjects:	TL500 Aeronautics TL787 Astronautics
Online Access:	http://irep.iium.edu.my/42772/ http://irep.iium.edu.my/42772/1/8%2877-88%2914-064.pdf http://irep.iium.edu.my/42772/4/42772-_wos%2Cscopus.pdf

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