最优鲁棒控制在飞行器设计中的应用  

THE APPLICATION OF OPTIMAL ROBUST CONTROL IN CONTROL SYSTEM DESIGN OF FLYING VEHICLES

作　　者：倪茂林[1] 王子才[2] 

机构地区：[1]北京控制工程研究所 [2]哈尔滨工业大学

出　　处：《宇航学报》1990年第3期23-27,共5页Journal of Astronautics

摘　　要：本文根据线性最优调节器加权阵与闭环系统极点的关系,提出了一种综合最优系统设计法,使系统同时具有良好的动特性和较强的鲁棒性。文中应用这种方法对某型飞行器控制系统进行了设计,使飞行器性能指标得到了显著提高。In this paper, based on the relation between the weighting matrices in linear quadratic optimal regulator and closed loop poles, a combined design method is presented for the optimal system with excellent dynamical characteristics and robustness. Applying this method in the design of control system of a certain flying vehicle,the performance is significantly improved.

关 键 词：导弹 鲁棒控制 最优调节器 设计 

分 类 号：TJ765.2[兵器科学与技术—武器系统与运用工程]