控制理论(社会学)
微分器
弹道
计算机科学
执行机构
国家观察员
自抗扰控制
参数化(大气建模)
跟踪(教育)
方案(数学)
特征向量
控制工程
控制(管理)
数学
带宽(计算)
工程类
人工智能
非线性系统
物理
数学分析
天文
心理学
辐射传输
量子力学
教育学
计算机网络
作者
Gaoqi Liu,Bin Li,Guang‐Ren Duan
出处
期刊:Guidance Navigation and Control
[World Scientific]
日期:2023-09-01
卷期号:03 (03)
被引量:24
标识
DOI:10.1142/s2737480723500152
摘要
In this paper, a fully actuated system approach (FASA)-based control scheme is proposed for the trajectory tracking of a quadrotor unmanned aerial vehicle (UAV). System uncertainty, external disturbance and actuator constraint are all considered, which make the problem challenging. Inspired by the active disturbance rejection control (ADRC), tracking differentiator (TD) and extended state observer (ESO) are introduced for handling the uncertainties and generating the feedback signals. With the proposed feedback control law, the performance of the resulted closed loop system is related to its eigenstructure - eigenvalue and eigenvectors. Based on a type of control parametrization method, the parametrized eigenstructure of the closed loop system are optimized. A better performance is observed by comparative numerical simulation.
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