Genetic algorithms for control of an aircraft-engine

被引：0

作者：

Fan, Ding ^{[1
]}

Fu, Qiang ^{[2
]}

Qi, Xue-Feng ^{[1
]}

机构：

[1] Coll. of Propulsion and Energy, Northwestern Polytechnical Univ., Xi'an 710072, China

[2] School of Flight Technique, Civil Aviation Flight Univ. of China, Guanghan 618307, China

来源：

Tuijin Jishu/Journal of Propulsion Technology | 2005年 / 26卷 / 06期

关键词：

Applications - Automation - Computer simulation - Control equipment - Control theory - Genetic algorithms - Performance - Propulsion - Three term control systems - Turbofan engines;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Due to its simplicity, utility and easy application, PID controller is used widely in classical automation systems. However, the performance of the PID controller cannot satisfy some systems which are complicated and nonlinear such as aircraft engines. This problem can be solved by the theory which is based on the genetic algorithms control theory. The integrated flight/propulsion control system of a fighter and its turbofan engine are studied. The genetic algorithms and PID control were combined which were used to revise the parameter of PID. The simulation results indicate that the designed integrated controller has good performances.

引用

页码：544 / 547