Robust attitude tracking control for a variable-pitch quadrotor with uncertainties

被引:1
|
作者
Zhao, Bo
Yue, Dong
Yang, Yang
机构
[1] Nanjing Univ Posts & Telecommun, Coll Automat, Nanjing, Jiangsu, Peoples R China
[2] Nanjing Univ Posts & Telecommun, Coll Artificial Intelligence, Nanjing, Jiangsu, Peoples R China
基金
中国国家自然科学基金;
关键词
hardware-in-the-loop (HIL); robust control; unmanned aerial vehicle (UAV); variable-pitch quadrotor; NONLINEAR CONTROL; FLIGHT; UAV;
D O I
10.1002/acs.3779
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Variable-pitch quadrotors have demonstrated their capability to enhance control performance and overcome limitations compared to conventional fixed-pitch quadrotors, while still facing challenges such as nonlinearity, couplings, uncertainties and so on. This article aims to address the robust attitude control problem of variable-pitch quadrotors afflicted with parametric uncertainties and unpredictable external disturbances. Initially, a practical actuator allocation strategy for the motor-propeller is proposed, followed by the development of a nonlinear robust attitude tracking controller capable of addressing all uncertainties. The effectiveness of the proposed controller in ensuring exponential stability of the closed-loop system, thereby driving the attitude tracking error to a small range within a finite time, has been substantiated. To evaluate the control performance, a hardware-in-the-loop testbed is constructed to conduct real-time experiments. The experimental results from attitude control case, comparative case, and position control case demonstrate that the designed motor-propeller allocation method and robust controller are effective in achieving a fast response and excellent control performance.
引用
收藏
页码:1878 / 1897
页数:20
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