DocumentCode
1597464
Title
Physical lumping methods for developing linear reduced models for high speed propulsion systems
Author
Immel, S.M. ; Hartley, T.T. ; de Abreu Garcia, J.A.
Author_Institution
Dept. of Electr. Eng., Akron Univ., OH, USA
fYear
1992
Firstpage
866
Abstract
A method that allows the development of both high-order large perturbation models and low-order small perturbation models of high-speed propulsion systems is presented. The large perturbation models have a clear nonlinear state space representation as compared with the usual computational fluid dynamics methods. The small perturbation models are easily obtained, given the propulsion system operating point. This modeling approach should be very useful in control system design and essentially parallels that developed by A. Chicatelli and T. T. Hartley (1990)
Keywords
aerospace propulsion; perturbation techniques; state-space methods; NASA Lewis 40-60 inlet; high speed propulsion systems; linear reduced models; nonlinear state space representation; perturbation models; Computational fluid dynamics; Control system synthesis; Difference equations; Digital simulation; Electric shock; Partial differential equations; Physics; Propulsion; Reduced order systems; State-space methods;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 1992., First IEEE Conference on
Conference_Location
Dayton, OH
Print_ISBN
0-7803-0047-5
Type
conf
DOI
10.1109/CCA.1992.269734
Filename
269734
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