节点文献
航空发动机多回路切换输出反馈控制的极点配置方法(英文)
Output Feedback Control of Aero-engine Multi-loops with Pole Placement Approach
【摘要】 通过利用极点配置的方法对多回路切换控制系统设计H∞输出反馈控制器。从复平面的一类凸区域的性质推导出控制器存在的充要条件,且以线性矩阵不等式的形式给出。最后,将设计方法运用到航空发动机多回路切换控制系统中,通过仿真可看出此方法是行之有效的。
【Abstract】 An approach was proposed which addressed the design of output feedback H ∞controllers. It satisfies the multi-loops switching control system on the closed-loop pole location. Sufficient and necessary conditions for feasibility were derived for a general class of convex regions of the complex plane. These conditions were expressed in terms of linear matrix inequalities (LMIs). Simulation results show the approach is feasible.
【关键词】 切换控制;
极点配置;
线性矩阵不等式;
航空发动机;
【Key words】 switching control; pole placement; linear matrix inequality; aero-engine;
【Key words】 switching control; pole placement; linear matrix inequality; aero-engine;
- 【文献出处】 系统仿真学报 ,Journal of System Simulation , 编辑部邮箱 ,2007年09期
- 【分类号】V233.7
- 【被引频次】6
- 【下载频次】249