Affiliation of Author(s):自动化学院
Journal:电子设计工程
Key Words:大柔性飞行器;模型参考自适应控制器;阵风扰动;姿态跟踪;
Abstract:大柔性飞行器是一类高空长航时飞行器,机翼展弦比大、柔性程度大。文中首先对非线性的大柔性飞行器模型进行线性化与降阶,之后对得到的模型进行模型参考自适应控制器的设计。在设计模型参考自适应控制律之前,首先设计线性二次型调节器(LQR)控制器,接着考虑不确定性,在LQR控制器的基础上,构造参考模型,设计模型参考自适应控制律。仿真结果显示,在阵风扰动下,模型参考自适应控制器能良好地跟踪俯仰角。
Translation or Not:no
Date of Publication:2018-09-20
Co-author:吕蓉蓉,xuliang,薛辰
Correspondence Author:lyp
Professor
Gender:Male
Alma Mater:南京航空航天大学
Education Level:With Certificate of Graduation for Study as Master's Candidates
Degree:Master's Degree in Engineering
School/Department:College of Automation Engineering
Discipline:Guidance, Navigation, and Control. Control Theory and Engineering. Control Science and Engineering
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