| 航空发动机结构参数和非结构参数不确定系统鲁棒H∞输出反馈控制 |
| |
| 引用本文： | 王曦,曾庆福.航空发动机结构参数和非结构参数不确定系统鲁棒H∞输出反馈控制[J].航空动力学报,1999,14(3). |
| |
| 作者姓名： | 王曦 曾庆福 |
| |
| 作者单位： | ：王曦 (北京航空航天大学) |
| |
| 摘 要： | The robust stability and robust
performance of aeroengine mixed uncertain system are analyzed.By introducing structured
singular value μ synthesis method,the robust H∞ output feedback control is
investigated under mixed structured and unstructured parameter perturbations.Disturbance
rejection and servo tracking performance with the designed controllers for aeroengine
uncertainty systems are simulated on a nonlinear model of twin-spool turbojet engine.
|
|
|
