论文部分内容阅读
具有良好的暂态响应的控制系统，其闭环系统的极点必须位于特定的区域。本文通过输出反馈，用三个线性矩阵不等式（ＬＭＩｓ）将线性定常系统的极点配置在左半平面一个圆域内。同时，针对一类线性变参数（ＬＰＶ）飞行器控制系统，通过一组ＬＭＩｓ用自调整输出反馈将该系统的极点配置到满足暂态性能要求的区域，为设计全包络线飞行器控制系统提供了理论基础。导弹系统仿真例子说明了该方法的可行性。
Control systems with good transient response must have the poles of the closed-loop system in a particular area. In this paper, we output the feedback and use the three linear matrix inequalities (LMIs) to arrange the poles of a linear steady-state system in a circle in the left half plane. At the same time, for a class of linear variable parameter (LPV) aircraft control system, the pole of the system is configured to meet the transient performance requirements through a set of LMIs with self-adjusting output feedback, which provides the design method for the full envelope aircraft control system Theoretical basis. The missile system simulation example illustrates the feasibility of this method.