- Title
- An adaptive regulation problem and its application to spacecraft systems
- Creator
- Chen, Zhiyong; Huang, Jie
- Relation
- 46th IEEE Conference on Decision and Control. Proceedings of the 46th IEEE Conference on Decision and Control (New Orleans, LA 12-14 December, 2007) p. 4631-4636
- Publisher Link
- http://dx.doi.org/10.1109/CDC.2007.4434122
- Publisher
- Institute of Electrical and Electronics Engineers (IEEE)
- Resource Type
- conference paper
- Date
- 2007
- Description
- The asymptotic rejection of spacecraft systems under multi-tone sinusoidal disturbances has been studied recently for the case where the frequencies are known. In this paper, we first consider an adaptive regulation problem of a class of uncertain nonlinear systems. Then an application of this result to the spacecraft systems leads to the solution of the asymptotic rejection of spacecraft systems subject to multi-tone sinusoidal functions with unknown frequencies.
- Subject
- adaptive control; attitude control; control systems; space vehicles
- Identifier
- http://hdl.handle.net/1959.13/937338
- Identifier
- uon:12550
- Identifier
- ISBN:9781424414970
- Rights
- Copyright © 2007 IEEE. Reprinted from the Proceedings of the 46th IEEE Conference on Decision and Control. This material is posted here with permission of the IEEE. Such permission of the IEEE does not in any way imply IEEE endorsement of any of University of Newcastle's products or services. Internal or personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution must be obtained from the IEEE by writing to pubs-permissions@ieee.org. By choosing to view this document, you agree to all provisions of the copyright laws protecting it.
- Language
- eng
- Full Text
- Reviewed
- Hits: 848
- Visitors: 1257
- Downloads: 255
| Thumbnail | File | Description | Size | Format | |||
|---|---|---|---|---|---|---|---|
| View Details Download | ATTACHMENT01 | Publisher version (open access) | 204 KB | Adobe Acrobat PDF | View Details Download |