Adaptive Neural Network PID Control for an Aeroengine

Jul. 2000

Article Contents

Article Navigation > Journal of Aerospace Power > 2000 > 15(3): 334-336

Jiang Yanjun, Huang Jinquan. Adaptive Neural Network PID Control for an Aeroengine[J]. Journal of Aerospace Power, 2000, 15(3): 334-336.

Citation:

Jiang Yanjun, Huang Jinquan. Adaptive Neural Network PID Control for an Aeroengine[J]. Journal of Aerospace Power, 2000, 15(3): 334-336.

Jiang Yanjun, Huang Jinquan. Adaptive Neural Network PID Control for an Aeroengine[J]. Journal of Aerospace Power, 2000, 15(3): 334-336.

Citation:

Jiang Yanjun, Huang Jinquan. Adaptive Neural Network PID Control for an Aeroengine[J]. Journal of Aerospace Power, 2000, 15(3): 334-336.

2nd Dept.NanJing University of Aeronautics and Astronautics,Nanjing 210016,China

Abstract

A multivariable adaptive neural network PID control scheme is proposed for a turbofan engine.The parameters of the controller are adjusted by on line conjugate gradient method.The precise model of the engine is not necessary for the design of the control system.The designed controller has many advantages such as fast response,strong interference free ability and good robustness.The control algorithm is simple,easy to realize and adaptable to full flight envelope.
- aeroengines,
- neural networks,