Multi-variable self-tuning control for aero-engines

被引：0

作者：

Pan, Mu-Xuan ^{[1
]}

Huang, Jin-Quan ^{[1
]}

机构：

[1] College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

来源：

Hangkong Dongli Xuebao/Journal of Aerospace Power | 2005年 / 20卷 / 05期

关键词：

Adaptive control systems - Closed loop control systems - Computer simulation - Identification (control systems) - Least squares approximations - Mathematical models - Multivariable control systems - Parameter estimation;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Based on the least square estimation with forgetting factor μ, the multi-variable self-tuning control was proposed for aero-engines with strong nonlinearity. The control parameters were obtained from estimation directly. The closed-loop control system was identifiable through the analysis. The simulation results show that the system features the rapid response, the high precision and the ability to restrain disturbance and coupling and the estimated parameters converge quickly.

引用

页码：868 / 872