DocumentCode
2702940
Title
Engine performance simulation using improved PSO algorithm
Author
Wang, Yonghua ; Zhu, Feixiang
Author_Institution
Grad. Students´´ Brigade, Naval Aeronaut. & Astronaut. Univ., Yantai, China
fYear
2012
fDate
15-18 June 2012
Firstpage
1410
Lastpage
1414
Abstract
Turbo fan engine mathematical model is a highly complex nonlinear system. Solving engine mathematical model with traditional iteration methods turns out to be difficult as these methods are very sensitive to initial values. Therefore particle swarm optimization is used to solve the model. An improved particle swarm optimization algorithm is produced. The mechanism of immune is introduced in the new algorithm. Clone selection mechanism based on Logistic chaotic mutation and diversity maintaining based on probability have been designed. Results show that the proposed algorithm has better searching performance and convergence speed than other compared algorithms when modeling a mixed exhaust turbofan engine.
Keywords
chaos; exhaust systems; iterative methods; jet engines; nonlinear control systems; particle swarm optimisation; performance evaluation; probability; search problems; PSO algorithm; clone selection mechanism; convergence speed; diversity maintenance; engine performance simulation; iteration methods; logistic chaotic mutation; mixed exhaust turbofan engine; nonlinear system; particle swarm optimization algorithm; probability; searching performance; turbo fan engine mathematical model; Algorithm design and analysis; Cloning; Engines; Equations; Mathematical model; Particle swarm optimization; Turbines; clone selection; engine; immune algorithm; particle swarm optimization; simulation;
fLanguage
English
Publisher
ieee
Conference_Titel
Quality, Reliability, Risk, Maintenance, and Safety Engineering (ICQR2MSE), 2012 International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4673-0786-4
Type
conf
DOI
10.1109/ICQR2MSE.2012.6246486
Filename
6246486
Link To Document