| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 721588 | IFAC Proceedings Volumes | 2007 | 6 Pages |
Abstract
The paper presents a stepwise procedure to develop a fault tolerant control system for small satellites. The procedure is illustrated through implementation on the AAUSAT-II spacecraft. As it is shown the presented procedure requires expertise from several disciplines that are nevertheless necessary for obtaining a complete and consistent solution.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
