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
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;
Conference_Titel :
Control Applications, 1992., First IEEE Conference on
Conference_Location :
Dayton, OH
Print_ISBN :
0-7803-0047-5
DOI :
10.1109/CCA.1992.269734