| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 717550 | IFAC Proceedings Volumes | 2012 | 6 Pages |
Abstract
This work proposes solutions for the Robust Static Output Feedback problem using optimization. The application considered is the design of flight control laws, taking into account structured uncertainties and flying qualities criteria, written in the μ robust control framework. An analysis of the resultant cost function is presented, some methods for solution are proposed and the results are discussed.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
