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).
This is the latest version of this item.
Full text not available from this repository.
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 Sciences and Engineering > Electronics and Computer Science
|Date Deposited:||02 Jun 2006|
|Last Modified:||27 Mar 2014 18:11|
|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]
Actions (login required)