涡扇发动机自增益调度H_∞控制器设计
Design of Self-Scheduled H_∞Control for Turbofan Engine
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摘要: 对可以用LPV(线性变参数)系统表示的涡扇发动机对象,将其凸分解为多胞表示,利用多胞特性将整个控制器设计转化为对胞体顶点控制器的设计。然后利用LMI(线性矩阵不等式)方法,对多胞的各顶点设计具有单一Lyapunov函数满足H∞性能且极点在给定区域的输出反馈控制器,综合顶点控制器得到具有同样多胞结构的全局连续变增益控制器。通过与一般的PID控制器进行对比验证了此控制器的有效性。Abstract: The LPV (Linear Parameter-Varying) system of turbofan engine was put into apolytopic expression by a convex decomposition,and the polytopic features were used to simplifythe controller design to a vertices' controller design.By using a LMI (Linear Matrix Inequality)approach,a feedback controller with the pole placement in a given region and with unique Lya-punov function for every vertex was designed, which satisfied H∞performance requirement.Aglobal continuous gain scheduled controller was then obtained by the synthesis of the vertex con-trollers.As compared with PID controller, the designed controller demonstrates its feasibility.
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Key words:
- aerospace propulsion system /
- turbofan engine /
- polytope /
- output feedback /
- gain scheduling /
- H∞control /
- pole placemen
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