Fixed-time robust trajectory tracking control for quadrotor UAV with disturbances

被引:4
|
作者
Shao, Shikai [1 ,2 ]
Wang, Shu [1 ]
Zhao, Yuanjie [1 ]
Huang, Gongfa [1 ]
机构
[1] Hebei Univ Sci & Technol, Sch Elect Engn, Shijiazhuang, Peoples R China
[2] Hebei Univ Sci & Technol, Sch Elect Engn, Shijiazhuang 050018, Peoples R China
关键词
Unmanned aerial vehicle; fixed-time stability; unknown input observer; extended state observer; bi-limit homogeneity; SLIDING MODE CONTROL; ADAPTIVE-CONTROL; LINEAR-SYSTEMS; CONTROL DESIGN; SPACECRAFT;
D O I
10.1177/01423312221123956
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Trajectory tracking control of nonlinear system with disturbances has been extensively investigated. A novel fixed-time robust trajectory tracking control scheme for quadrotor unmanned aerial vehicle (UAV) with disturbances is proposed in this paper. First, the quadrotor system is split into position and attitude loops. With the purpose of restraining coupling disturbances on position loop forced by imperfect attitude tracking, a novel fixed-time unknown input observer (UIO) is devised to accurately estimate the disturbances, with the unique feature that does not need the upper bound of disturbances or the derivatives. Second, taking unmeasurable velocity and unknown external disturbances into account for attitude loop, a fixed-time extended state observer (ESO) is proposed to precisely observe them within a fixed time. Third, considering control accuracy and convergence rate, robust fixed-time controllers are, respectively, designed for position and attitude loops, and the convergence time of overall system is independent of system initial states. Then, a comprehensive stability proof for the two-loop system is presented with a combination of bi-limit homogeneity and Lyapunov technique. Finally, simulations and comparisons are performed to demonstrate the effectiveness of the designed control scheme.
引用
收藏
页码:1213 / 1228
页数:16
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