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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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)|
|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 and Applied Science > Electronics and Computer Science
|Date Deposited:||02 Jun 2006|
|Last Modified:||25 Apr 2013 11:11|
|Contributors:||Veres, S.M. (Author)
Gabriel, S.B. (Author)
Rogers, E. (Author)
Mayne, D.Q. (Author)
|Further Information:||Google Scholar|
|ISI Citation Count:||2|
|RDF:||RDF+N-Triples, RDF+N3, RDF+XML, Browse.|
Available Versions of this Item
Analysis of Formation Flying Control of a Pair of Nano-satellites. (deposited 05 Mar 2002)
- Analysis of formation flying control of a pair of nano-satellites. (deposited 02 Jun 2006) [Currently Displayed]
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