DocumentCode :
3021260
Title :
A nonlinear approach to the design of jet engine control systems
Author :
Sridhar, B. ; Calise, A.J.
Author_Institution :
Dynamics Research Corporation, Wilmington, Massachusetts
fYear :
1977
fDate :
7-9 Dec. 1977
Firstpage :
1181
Lastpage :
1185
Abstract :
This paper uses a multiple time scaling analysis of jet engine dynamics to derive a non-linear minimum time control law. The ideas are based on concepts taken from singular perturbation theory. Further reductions in model order are permitted by this approach, which results in a feedback form for the control solution. Numerical results are given which compare the accuracy of the solution with open-loop solutions obtained using conjugate gradient and dynamic programming methods.
Keywords :
Aerodynamics; Aerospace control; Aircraft; Compressors; Control systems; Feedback control; Jet engines; Nonlinear control systems; Open loop systems; Time factors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control including the 16th Symposium on Adaptive Processes and A Special Symposium on Fuzzy Set Theory and Applications, 1977 IEEE Conference on
Conference_Location :
New Orleans, LA, USA
Type :
conf
DOI :
10.1109/CDC.1977.271749
Filename :
4046019
Link To Document :
بازگشت