Ellipsoid methods for formation flying control of two nano-satellites
Veres, S.M., Rokitianski, D.Y., Gabriel, S.B. and Rogers, E. (2002) Ellipsoid methods for formation flying control of two nano-satellites. In, Proceedings of the International Conference on Control Applications, 2002. International Conference on Control Applications 2002 Piscataway, US, Institute of Electrical and Electronics Engineers, 298-303. (doi:10.1109/CCA.2002.1040202).
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Description/Abstract
The paper provides analysis and implementable ellipsoid-based solutions to the constrained control problems of stabilization and manoeuvre control of two nano-satellites. The solutions under ellipsoid constraints of actuators and measurements are considered, covering input magnitude constraints, bounded disturbances and measurement errors. An example illustrates the presented method with simulation of the motion of a nano-satellite pair.
| Item Type: | Book Section |
|---|---|
| ISBNs: | 0780373863 (hardback) |
| Subjects: | T Technology > TL Motor vehicles. Aeronautics. Astronautics |
| Divisions: | Faculty of Physical and Applied Science > Electronics and Computer Science > Comms, Signal Processing & Control Faculty of Engineering and the Environment > Engineering Sciences |
| Item ID: | 257482 |
| Date Deposited: | 03 Mar 2004 |
| Last Modified: | 26 Apr 2013 02:50 |
| Contributors: | Veres, S.M. (Author) Rokitianski, D.Y. (Author) Gabriel, S.B. (Author) Rogers, E. (Author) |
| Date: | 2002 |
| Status: | Published |
| Publisher: | Institute of Electrical and Electronics Engineers |
| Further Information: | Google Scholar |
| ISI Citation Count: | 1 |
| URI: | http://eprints.soton.ac.uk/id/eprint/257482 |
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