DocumentCode
3370337
Title
Optimum performance seeking control of aero-engine based on Sequential Quadratic Programming
Author
Xiu-ling, Xu ; Xiao-dong, Wang
Author_Institution
Coll. of Math., Phys. & Inf. Eng., Zhejiang Normal Univ., Jinhua, China
fYear
2010
fDate
26-28 June 2010
Firstpage
5994
Lastpage
5996
Abstract
A methodology based on the nonlinear algorithm of Sequential Quadratic Programming in engine performance seeking control is presented. This article is aimed at analyzing the inherent limitation and max-acceleration. Simulation result shows that the engine has better acceleration performance through seeking control, and Sequential Quadratic Programming is suitable for the Optimum performance seeking control of engine, and SQP is suitable for the optimum performance seeking of engine.
Keywords
aerospace engines; nonlinear control systems; optimal control; performance index; quadratic programming; aeroengine; engine performance seeking control; nonlinear algorithm; optimum performance seeking control; sequential quadratic programming; Acceleration; Cities and towns; Educational institutions; Engines; Mathematics; Physics; Quadratic programming; Tellurium; aero-engine; optimum performance; sequential quadratic programming;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechanic Automation and Control Engineering (MACE), 2010 International Conference on
Conference_Location
Wuhan
Print_ISBN
978-1-4244-7737-1
Type
conf
DOI
10.1109/MACE.2010.5536858
Filename
5536858
Link To Document