计算机与现代化Issue(6)：1-4,4.DOI:10.3969/j.issn.1006-2475.2013.06.001
高超声速飞行器自抗扰控制方法研究
Active Disturbance Rejection Control for Airbreathing Hypersonic Vehicle
摘要
Abstract
Hypersonic vehicle requires strictly for angle of attack and angle of sideslip when its engine is working.To meet the requirements,angle of attack autopilot is designed with auto-disturbance rejection control.The system's state and the disturbance are estimated using the extended state observer.The state error is feedbacked nonlinearly and the disturbance is compensated in order to trace the dictates accurately.With the result of the simulation,it is shown that this method of control can reject the disturbance and meets the requirements well.关键词
高超声速飞行器/自抗扰控制/攻角控制Key words
hypersonic vehicle/active disturbance rejection/angle of attack control分类
航空航天引用本文复制引用
杜昊昱,凡永华,闫杰..高超声速飞行器自抗扰控制方法研究[J].计算机与现代化,2013,(6):1-4,4.基金项目
国家自然科学基金资助项目(90816027) （90816027）
