DocumentCode :
3071221
Title :
Application of the extended linearization design method to longitudinal flight control
Author :
Baumann, W.T. ; Wang, J.L. ; Rugh, W.J.
Author_Institution :
The Johns Hopkins University, Baltimore, Maryland
fYear :
1985
fDate :
11-13 Dec. 1985
Firstpage :
1653
Lastpage :
1653
Abstract :
A typical approach to control of a nonlinear system is to linearize the system about a nominal operating point. Then linear feedback design methods are used, yielding a closed-loop system whose linearization about the corresponding closed-loop operating point has the desired characteristics. So long as the closed-loop system is operated in a region sufficiently close to the operating point, the closed-loop linearization should accurately reflect the behavior of the closed-loop nonlinear system. Of course, simulation is used to verify the design effectiveness.
Keywords :
Aerospace control; Control system synthesis; Control systems; Design methodology; Feedback control; Linear feedback control systems; Nonlinear control systems; Nonlinear systems; Optimal control; Output feedback;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1985 24th IEEE Conference on
Conference_Location :
Fort Lauderdale, FL, USA
Type :
conf
DOI :
10.1109/CDC.1985.268796
Filename :
4048596
Link To Document :
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