Robust control of a laboratory flight simulator by nondynamic multirate output feedback

Publikationstyp
Conference Paper
Date Issued
1996
Sprache
English
Author(s)
Werner, Herbert  
TORE-URI
http://hdl.handle.net/11420/14727
Start Page
1575
End Page
1580
Citation
Proceedings of the 35th IEEE Conference on Decision and Control. - Piscataway, NJ, 1996. - Vol. 2 (): 1575-1580 (1996)
Contribution to Conference
35th IEEE Conference on Decision and Control, CDC 1996  
Publisher DOI
10.1109/CDC.1996.572749
Scopus ID
2-s2.0-0030389509
Publisher
IEEE
This paper describes the application of a new nondynamic multirate output feedback control law to a robust tracking problem for an unstable plant. The nonlinear plant is linearized around its nominal operating point and around two possible failure modes. The controller design is carried out in two steps: convex programming methods can be used to find a state feedback gain which meets given specifications in the nominal operating point and under failure conditions. Then this state feedback gain is realized by a multirate output feedback control law. Experimental results show that this output feedback controller maintains the performance achieved by state feedback.
DDC Class
600: Technik
620: Ingenieurwissenschaften