Analysis of formation flying control of a pair of nano-satellites
Analysis of formation flying control of a pair of nano-satellites
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.
constrained control problems, differential drag, disturbances, formation flying control, magnitude constraints, maneuver control, measurement errors, nano-satellites, propulsion, stabilization
0780370619
1095-1100
Veres, S.M.
909c60a0-56a3-4eb6-83e4-d52742ecd304
Gabriel, S.B.
ac76976d-74fd-40a0-808d-c9f68a38f259
Rogers, E.
611b1de0-c505-472e-a03f-c5294c63bb72
Mayne, D.Q.
f4bd5584-4ef0-4cbb-be7a-8be43696ff4c
December 2001
Veres, S.M.
909c60a0-56a3-4eb6-83e4-d52742ecd304
Gabriel, S.B.
ac76976d-74fd-40a0-808d-c9f68a38f259
Rogers, E.
611b1de0-c505-472e-a03f-c5294c63bb72
Mayne, D.Q.
f4bd5584-4ef0-4cbb-be7a-8be43696ff4c
Veres, S.M., Gabriel, S.B., Rogers, E. and Mayne, D.Q.
(2001)
Analysis of formation flying control of a pair of nano-satellites.
Proceedings of the 40th IEEE Conference on Design and Control, 2001, Orlando, United States.
04 - 07 Dec 2001.
.
(doi:10.1109/.2001.981031).
Record type:
Conference or Workshop Item
(Paper)
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.
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More information
Published date: December 2001
Venue - Dates:
Proceedings of the 40th IEEE Conference on Design and Control, 2001, Orlando, United States, 2001-12-04 - 2001-12-07
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
ISBN: 0780370619
PURE UUID: daadc430-3b74-4ab7-b2c0-2bcec180792b
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Date deposited: 02 Jun 2006
Last modified: 16 Mar 2024 02:41
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Contributors
Author:
S.M. Veres
Author:
S.B. Gabriel
Author:
E. Rogers
Author:
D.Q. Mayne
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