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:
Online Access:http://irep.iium.edu.my/42772/1/8%2877-88%2914-064.pdf
http://irep.iium.edu.my/42772/4/42772-_wos%2Cscopus.pdf
http://irep.iium.edu.my/42772/
http://ijass.org/On_line/admin/files/8(77~88)14-064.pdf
http://dx.doi.org/10.5139/IJASS.2015.16.1.77
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