DocumentCode
2434835
Title
Embedding FDI in launcher attitude controllers
Author
Ramos, Fausto ; Alazard, Daniel
Author_Institution
ISAE, Univ. de Toulouse, Toulouse, France
fYear
2009
fDate
11-13 June 2009
Firstpage
609
Lastpage
614
Abstract
It looks interesting the idea of obtaining more than a controller after designing a control system. In fact, given some conditions, it is possible to rearrange the controller states, revealing an observer structure, without changing the original system. Such proposition does not only means that the estimations of the plant states are available, but also that fault estimators can be built, providing an unexpected horizon of fault tolerance and even control reconfiguration. In order to illustrate that, a generalization aimed at obtaining observer-based forms from augmented, reduced or full order controllers will be applied to a launcher model, subject to sensor faults and external disturbance.
Keywords
attitude control; control system synthesis; fault diagnosis; fault tolerance; observers; state estimation; FDI; control system design; even control reconfiguration; fault detection-and-isolation; fault tolerance; launcher attitude controller; observer structure; plant state estimation; Aerospace control; Attitude control; Control systems; Fault detection; Fault tolerance; Nonlinear control systems; Observers; Robust control; Robust stability; State estimation;
fLanguage
English
Publisher
ieee
Conference_Titel
Recent Advances in Space Technologies, 2009. RAST '09. 4th International Conference on
Conference_Location
Istanbul
Print_ISBN
978-1-4244-3627-9
Electronic_ISBN
978-1-4244-3628-6
Type
conf
DOI
10.1109/RAST.2009.5158264
Filename
5158264
Link To Document