Title :
Neural networks adaptive control of aircraft engine based on genetic algorithm
Author :
Hongmei Zhang ; Ziyun Dong ; Guangyan Xu
Author_Institution :
Aerosp. Fac., Shenyang Aerosp. Univ., Shenyang, China
fDate :
May 31 2014-June 2 2014
Abstract :
In this paper, a method of neural network adaptive control was proposed based on genetic algorithm (GA). At first, genetic algorithm is applied to determine initial weights of neural networks (NNs), and then NNs identifier is applied to real-time identify the model of engine. Moreover, the sensitivity information of the system is fed back to the NNs controller, which ensures the accuracy of the controller for the controlled object. For an aircraft turbojet engine, the control system is designed on the selected design point. The simulation results show that the control system not only has good quickness and less overshoot but also has strong anti-interference ability.
Keywords :
adaptive control; aircraft control; genetic algorithms; jet engines; neurocontrollers; NN controller; NN identifier; adaptive control; aircraft turbojet engine; antiinterference ability; genetic algorithm; neural network; sensitivity information; Adaptive control; Aircraft propulsion; Artificial neural networks; Control systems; Engines; Genetic algorithms; Aircraft Engine; Genetic Algorithm; Neural Networks; Self-adaptation Control;
Conference_Titel :
Control and Decision Conference (2014 CCDC), The 26th Chinese
Conference_Location :
Changsha
Print_ISBN :
978-1-4799-3707-3
DOI :
10.1109/CCDC.2014.6852788