火力与指挥控制2017，Vol.42Issue(3)：161-165,5.
基于反馈解耦法的旋转火箭弹自适应控制系统设计
Design of Adaptive Control System for Spinning Rockets Based on Feedback Decoupling Method
摘要
Abstract
The spinning of rockets will cause strong coupling between pitch and yaw channel and the kinetic parameters of rockets are changing significantly during flight,which will make it more difficult to design the control system for spinning rockets. For the coupling of two channels,the feedback method is applied to achieve dynamic decoupling and the model reference adaptive control (MARC) method is used to design the controller for every single channel. The results show that the above methods can reduce the impact of coupling on control system and improve robustness of control system against the changes of kinetic parameters and external disturbance as well as satisfy the requirements of flight control system for spinning rockets.关键词
旋转火箭弹/反馈解耦/自适应控制/鲁棒性Key words
spinning rockets/feedback decoupling/adaptive control/robustness分类
军事科技引用本文复制引用
阮政委,周文雅,张大力,秦黎博..基于反馈解耦法的旋转火箭弹自适应控制系统设计[J].火力与指挥控制,2017,42(3):161-165,5.基金项目
航空科学基金资助项目(20130163002) （20130163002）
