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满足二次稳定性的航空发动机H_∞控制器设计
DESIGN OF AEROENGINE H_∞ CONTROLLER OF SATISFING QUADRATIC STABILITY
【摘要】 对于一类输出矩阵存在结构参数摄动的对象, 提出了闭环系统满足二次稳定性的H∞输出动态反馈控制器的理论设计方法。随后进行了同时满足二次稳定及干扰抑制性能指标的H∞控制器设计, 最后的仿真结果表明所设计的控制系统具有较好的稳定鲁棒性及动态性能
【Abstract】 To a class of structured perturbation plants about which state and output matrixes are uncertain,a sufficient and necessary condition is presented to the quadratic stability via H ∞ dynamic output feedback controller.To make the system be of the quadratic stability and satisfy quadratic performance,a controller is designed later.The simulation shows that the control system designed is of good stable robustness and dynamic performance.
【关键词】 航空发动机;
系统稳定性;
闭环控制;
H_∞控制;
结构参数;
摄动;
【Key words】 Aircraft engine; System stability; Closed loop control; H_∞ control +; Structure parameter; Perturbation;
【Key words】 Aircraft engine; System stability; Closed loop control; H_∞ control +; Structure parameter; Perturbation;
- 【文献出处】 推进技术 ,JOURNAL OF PROPULSION TECHNOLOGY , 编辑部邮箱 ,1999年05期
- 【分类号】V233.73
- 【下载频次】56