| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 714503 | IFAC Proceedings Volumes | 2013 | 6 Pages |
Abstract
An optimal input design technique for aircraft uncertain parameter estimation is presented in this paper. The original idea is the combining of a dynamic programming method and interval analysis for the optimal input synthesis. This approach does not imply the estimation of a nominal value for parameter and allows to include realistic practical constraints on the input and output variables. The precise description of the approach is followed by an application in aerospace sciences.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
