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 :
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