Finite-Time Geometric Tracking Controller for Multirotor Systems

被引:1
作者
An, Han-Hsuan [1 ]
Cheng, Teng-Hu [1 ]
机构
[1] Natl Yang Ming Chiao Tung Univ, Dept Mech Engn, Hsinchu 30010, Taiwan
关键词
Convergence; Angular velocity; Stability criteria; Attitude control; Asymptotic stability; Symbols; Aerospace electronics; Nonlinear control; Lyapunov methods; Tracking; Finite-time stability; geometric tracking control; disturbance compensator; nonlinear control; Lyapunov theory; SLIDING MODE CONTROL; ATTITUDE TRACKING; STABILITY; DESIGN; HOMOGENEITY;
D O I
10.1109/ACCESS.2022.3215689
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
A continuous nonsingular terminal sliding-mode controller (N-TSMC) has been developed that ensures finite time convergence of the attitude of a multirotor subject to disturbance. A newly designed disturbance compensator is incorporated in the developed controller to guarantee that the disturbance compensation error exhibits finite-time convergence. A stability analysis showed that the developed controller can ensure that the closed-loop system achieves homogeneous finitetime stability. Simulations were performed to verify the efficacy of the developed controller. Compared with the traditional NTSMC, the simulation results indicate that the continuous NTSMC can still achieve finite-time convergence without causing high-frequency chattering since the control input is continuous. To the best of our knowledge, this is the first time that a continuous N-TSMC has been applied to multirotor systems to ensure finite-time stability.
引用
收藏
页码:110905 / 110915
页数:11
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