DocumentCode
425708
Title
Control design decoupling for two-way coupled systems
Author
Ruiter, A. H J De ; Liu, Hugh H. T.
Author_Institution
Inst. for Aerosp. Studies, Toronto Univ., Downsview, Ont., Canada
Volume
1
fYear
2004
fDate
2-4 Sept. 2004
Firstpage
776
Abstract
Many systems are made up of a number of interacting subsystems, with multiple performance specifications to be met. For such systems, the control system design becomes a challenging task. Conventional engineering process follows a bottom-up approach, where the subsystem controllers are designed independently, and then the subsystems are assembled. Unaccounted for interactions are then handled by ad-hoc troubleshooting methods, which may compromise the original design specifications. We present a design decoupling method such that the resulting closed-loop system and its overall system performance is achieved by the subsystem controller implementation. The subsystem controller design is treated as if they are independent. Therefore, the system integration process is straight forward and the performance (including subsystem interactions) has been systematically addressed.
Keywords
closed loop systems; control system synthesis; decentralised control; ad hoc troubleshooting methods; closed loop system; control system design decoupling method; conventional engineering process; subsystem controller design; subsystem interaction; system integration process; two way coupled systems; Actuators; Aerospace engineering; Aircraft propulsion; Assembly; Centralized control; Control design; Control systems; Design engineering; Design methodology; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 2004. Proceedings of the 2004 IEEE International Conference on
Print_ISBN
0-7803-8633-7
Type
conf
DOI
10.1109/CCA.2004.1387308
Filename
1387308
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