Autonomous multi satellites assembly in keplerian orbits

In this paper, the guidance and control algorithms of an autonomous multiple satellite assembly are developed in a general keplerian orbit. The guidance algorithms are based on defining the velocity profile of each satellite in two different segment of space. In the first segment, the guidance law u...

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Bibliographic Details
Main Authors: Okasha, Mohamed Elsayed Aly Abd Elaziz, Park, Chandeok, Park, Sang-Young
Format: Conference or Workshop Item
Language:English
Published: American Institute of Aeronautics and Astronautics 2013
Subjects:
Online Access:http://irep.iium.edu.my/38417/
http://irep.iium.edu.my/38417/
http://irep.iium.edu.my/38417/
http://irep.iium.edu.my/38417/1/Autonomous_Multi_Satellites_Assembly_in_Keplerian_Orbits.pdf