计算机与现代化Issue(7)：105-108,4.DOI:10.3969/j.issn.1006-2475.2013.07.028
空射巡航导弹H∞/混合灵敏度控制器设计
H∞/Mixed Sensitivity Controller Design for Airlaunched Cruise Missile
樊朋飞 1凡永华 1于云峰1
作者信息
- 1. 西北工业大学航天学院,陕西西安710072
- 折叠
摘要
Abstract
For the large height span and dramatic changes in the model parameters of airlaunched cruise missile during the whole process from launching to hitting ground target,and the request for sideslip angle of BTT control,using H∞/Mixed sensitivity design method,this paper describes the parameter variations as multiplicative uncertainty in the output,the robust controller is designed based on three-channel decoupling model of the missile.The simulation results show that the designed controller is able to ensure strong stability and well time-domain response performance to the selected different characteristic points throughout the flight trajectory of cruise missile,inhibit lateral overload effectively in the process of turning,and achieve the goal of limiting sideslip angle.关键词
空射巡航导弹/倾斜转弯/鲁棒控制/混合灵敏度Key words
airlaunched cruise missile/bank-to-turn/robust control/mixed sensitivity分类
军事科技引用本文复制引用
樊朋飞,凡永华,于云峰..空射巡航导弹H∞/混合灵敏度控制器设计[J].计算机与现代化,2013,(7):105-108,4.
