基于ESO的BTT飞行器多变量解耦控制方法研究  

Multivariable Decoupling Control Method of BTT Aircraft Based on ESO

作　　者：杜立夫[1] 张瑞[1] 赵志芳[1] 闵勇[1] DU Lifu;ZHANG Rui;ZHAO Zhifang;MIN Yong(Beijing Aerospace Automatic Control Institute,Beijing 100854,China)

机构地区：[1]北京航天自动控制研究所,北京100854

出　　处：《上海航天》2018年第1期81-86,共6页Aerospace Shanghai

基　　金：国家自然科学基金青年科学基金(61403355)

摘　　要：针对倾斜转弯(BTT)飞行器姿态控制系统的多变量耦合问题,提出一种基于扩张状态观测器(ESO)的多变量解耦控制方法。将BTT飞行器系统中的耦合视为扰动,利用ESO具有实时跟踪估计扰动能力的特点,将耦合扰动估计出来,通过补偿消除耦合的影响。利用极点配置的方法完成闭环状态反馈控制律设计,并通过数学仿真验证方法的正确性和有效性。Considering that multivariable coupling problem of bank to turn(BTT)aircraft attitude control system,a multivariable method based on extended state observer(ESO)is proposed.The coupling in the BTT aircraft system is considered as interference,the coupling disturbance is tracked and estimated in real time by ESO,and the coupling effect is eliminated by compensation.The closed loop state feedback control law is designed by means of polar assignment.The correctness and effectiveness of the method are verified by mathematical simulation.

关 键 词：倾斜转弯飞行器 姿态控制 自抗扰控制器 扩张状态观测器 多变量系统 解耦控制 极点配置 三通道独立设计 

分 类 号：V448.2[航空宇航科学与技术—飞行器设计]