Disturbance Observer-Based Singularity-Free Predefined-Time Attitude Tracking Control of Quadrotors: Theory and Experiments

被引:2
作者
Zhang, Zhihao [1 ,4 ,5 ]
Xie, Shuzong [2 ,6 ]
Chen, Qiang [3 ,4 ]
机构
[1] China Beihang Univ, Zhejiang Univ Technol, Hangzhou, Beijing, Peoples R China
[2] Zhejiang Univ Sci Technol, Hangzhou, Peoples R China
[3] Zhejiang Univ Technol, Hangzhou, Peoples R China
[4] Zhejiang Univ Technol, Coll Informat Engn, Data Driven Intelligent Syst Lab, Hangzhou 310023, Peoples R China
[5] Beihang Univ, Inst Unmanned Syst, Beijing 100083, Peoples R China
[6] Zhejiang Univ Sci & Technol, Sch Automat & Elect Engn, Hangzhou 310023, Peoples R China
基金
中国国家自然科学基金;
关键词
Quadrotors; Convergence; Attitude control; Upper bound; Disturbance observers; Aerospace and electronic systems; Electronic mail; Attitude tracking; disturbance observer (DOB); predefined-time convergence; quadrotors; singularity-free sliding mode control; RIGID SPACECRAFT; HOVERING CONTROL; STABILIZATION;
D O I
10.1109/TAES.2024.3446754
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this article, a disturbance observer-based singularity-free attitude tracking control scheme is presented for quadrotors. First, a predefined-time disturbance observer is constructed to estimate and compensate for external disturbances, enabling the fast convergence of disturbance estimation. Then, a singularity-free predefined-time sliding mode surface is devised with the directly nonsingular property, and an auxiliary function is introduced in the controller design process to avoid the potential singularity problem. On this basis, a predefined-time controller without singularity is proposed to drive the attitude tracking errors to the origin within an expected convergence time. Unlike the majority of existing predefined-time control schemes, this work circumvents the singularity problem without relying on continuous piecewise functions or quadratic-fraction functions, resulting in a more concise and clear stability analysis. Finally, three different control schemes are implemented for experimental comparison, and the results confirm the effectiveness of the proposed control scheme.
引用
收藏
页码:314 / 324
页数:11
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