| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 5003095 | IFAC-PapersOnLine | 2016 | 6 Pages |
Abstract
In this paper, the feasibility of structured Hâ control design is demonstrated in representative environment for flexible launcher control during non-stationary ascent phase. Robust control is achieved and performances are improved with respect to non structured Hâ controller; furthermore, numerous simplifications in control design process are highlighted providing flight control development cost reduction perspectives. These results pave the way towards industrial application of structured Hâ framework for existing and future European launcher control. Further research axes are currently under investigation in the frame of co-funded AIRBUS DS and CNES researches.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
Authors
M. Ganet-Schoeller, Jean Desmariaux,