Analysis of formation flying control of a pair of nano-satellites


Veres, S.M., Gabriel, S.B., Rogers, E. and Mayne, D.Q. (2001) Analysis of formation flying control of a pair of nano-satellites. In, Proceedings of the 40th IEEE Conference on Design and Control, 2001, Orlando, US, 04 - 07 Dec 2001. , 1095-1100. (doi:10.1109/.2001.981031).

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Original Publication URL: http://dx.doi.org/10.1109/.2001.981031

Description/Abstract

This paper gives an analysis and provides implementable solutions for constrained control problems of stabilization and maneuver control of two nano-satellites. The methodology provides solutions under various constraints of propulsion and differential drag control: magnitude constraints, disturbances and measurement errors are taken into account. The methods are illustrated in simulation of a realistic nano-satellite pair.

Item Type: Conference or Workshop Item (Paper)
ISBNs: 0780370619
Related URLs:
Keywords: constrained control problems , differential drag , disturbances, formation flying control, magnitude constraints, maneuver control, measurement errors, nano-satellites, propulsion, stabilization
Subjects: Q Science > QA Mathematics > QA75 Electronic computers. Computer science
T Technology > TL Motor vehicles. Aeronautics. Astronautics
Divisions: University Structure - Pre August 2011 > School of Engineering Sciences
Faculty of Engineering and the Environment
Faculty of Physical Sciences and Engineering > Electronics and Computer Science
ePrint ID: 22001
Date Deposited: 02 Jun 2006
Last Modified: 27 Mar 2014 18:11
Further Information:Google Scholar
ISI Citation Count:2
URI: http://eprints.soton.ac.uk/id/eprint/22001

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