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

Record type: Conference or Workshop Item (Paper)

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.

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Citation

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

More information

Published date: December 2001

Venue - Dates: Proceedings of the 40th IEEE Conference on Design and Control, 2001, United States, 2001-12-04 - 2001-12-07

Related URLs:

http://www.ecs.umass.edu/cdc2001/

Keywords: constrained control problems, differential drag, disturbances, formation flying control, magnitude constraints, maneuver control, measurement errors, nano-satellites, propulsion, stabilization

Organisations: Electronics & Computer Science, Faculty of Engineering and the Environment

Identifiers

Local EPrints ID: 22001

URI: http://eprints.soton.ac.uk/id/eprint/22001

DOI: doi:10.1109/.2001.981031

ISBN: 0780370619

PURE UUID: daadc430-3b74-4ab7-b2c0-2bcec180792b

Catalogue record

Date deposited: 02 Jun 2006

Last modified: 17 Jul 2017 16:24

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Contributors

Author: S.M. Veres

Author: S.B. Gabriel

Author: E. Rogers

Author: D.Q. Mayne

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