Optimization Methodology of PI Controller Parameters for Aeroengines Based on Genetic Algorithm
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Optimization Methodology of PI Controller Parameters for Aeroengines Based on Genetic Algorithm
Vol. 20, Issue 6, (2005)
作者机构:
1. 南京航空航天大学能源与动力学院,江苏,南京,210016
2. 中航第一集团公司航空动力控制系统研究所,江苏,无锡,214063
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Published:2005
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SU Wei-sheng, LI Yue, SUN Jian-guo, et al. Optimization Methodology of PI Controller Parameters for Aeroengines Based on Genetic Algorithm[J]. 2005, 20(6).
DOI:
SU Wei-sheng, LI Yue, SUN Jian-guo, et al. Optimization Methodology of PI Controller Parameters for Aeroengines Based on Genetic Algorithm[J]. 2005, 20(6).DOI:
Optimization Methodology of PI Controller Parameters for Aeroengines Based on Genetic Algorithm
an optimization methodology of the PI controller parameters with Genetic Algorithm(GA)was developed.This optimization methodology is a global optimization and has nothing to do with initial values.The fitting function used was based on the weighting combination of the system dynamic and steady state performance.The PI controller parameters of an aeroengine for both single-input single-output and two-input two-output were optimized with GA.The simulation results indicate that the optimization methodology of the aeroengine PI controller parameters developed in this paper is very effective.