微型飞行器
拍打
翼
线性化
非线性系统
跟踪误差
空气动力学
控制理论(社会学)
航空航天工程
理论(学习稳定性)
航程(航空)
计算机科学
工程类
控制(管理)
人工智能
物理
机器学习
量子力学
作者
Zunyao Yang,Zhongsheng Hou,Shangtai Jin
摘要
Abstract In this paper, two robust model‐free adaptive control (RMFAC) methods are proposed for a nonlinear flapping wing micro air vehicle (FWMAV) subject to measurable and unmeasurable wind disturbances. Firstly, a novel disturbance‐related full‐form dynamic linearization technique (DFFDL) is developed to transform the FWMAV with measurable disturbances into a dynamic linearization data model. Then, a DFFDL based RMFAC method is designed based on the obtained data model for the FWMAV to suppress the wind disturbances. Next, the stability analysis shows that the system output tracking error converges into a bounded range. And the above result is extended to the case of unmeasurable disturbances. Finally, the simulation comparison results demonstrate the effectiveness of two proposed RMFAC methods.
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