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
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;
Conference_Titel :
Mechanic Automation and Control Engineering (MACE), 2010 International Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-7737-1
DOI :
10.1109/MACE.2010.5536858
