Referenced Items are not available for this document.
The problem of designing discrete-time attitude controllers for three-axis stabilization of magnetically actuated spacecraft is considered. Several methods are discussed and an approach to the tuning of various classes of projection-based controllers is proposed relying on periodic optimal output feedback control techniques. The main advantages of the proposed methods are discussed and illustrated in a simulation study.
Published in:
Control Systems Technology, IEEE Transactions on
(Volume:18
,
Issue:
3
)
Date of Publication: May 2010
- Page(s):
- 714 - 722
- ISSN :
- 1063-6536
- INSPEC Accession Number:
- 11260203
- Digital Object Identifier :
- 10.1109/TCST.2009.2024757
- Product Type:
- Journals & Magazines
- Date of Publication :
- 11 August 2009
- Date of Current Version :
- 22 April 2010
- Issue Date :
- May 2010
- Sponsored by :
- IEEE Control Systems Society
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