Event-Triggered Finite-Time Attitude Cooperative Control for Multiple Unmanned Aerial Vehicles
Author(s) -
Qiang Han,
Yongshuai Zhou,
Xin Liu,
Xianguo Tuo
Publication year - 2022
Publication title -
applied bionics and biomechanics
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.397
H-Index - 23
eISSN - 1754-2103
pISSN - 1176-2322
DOI - 10.1155/2022/5875004
Subject(s) - control theory (sociology) , quaternion , lyapunov stability , controller (irrigation) , attitude control , lyapunov function , mode (computer interface) , stability (learning theory) , computer science , invertible matrix , singularity , zeno's paradoxes , angular velocity , scheme (mathematics) , terminal sliding mode , control (management) , engineering , control engineering , sliding mode control , mathematics , artificial intelligence , nonlinear system , mathematical analysis , physics , geometry , quantum mechanics , machine learning , pure mathematics , agronomy , biology , operating system
The finite-time attitude cooperative control problem for a group of multiple unmanned aerial vehicle systems with external disturbances and uncertain parameters is discussed in this paper. The dynamics of the systems is described by quaternion avoiding the singularity. Based on the attitude error and angular velocity error, a novel nonsingular terminal sliding mode surface is proposed for the controller with event-triggered scheme. The lumped disturbances are estimated by neural networks with adaptive law. The communication frequency is decreased by the proposed distributed event-triggered based sliding mode controller. Lyapunov theory is utilized to analyze the stability of the systems, and the Zeno behavior is avoided by rigorous proof. Finally, simulation examples are presented to illustrate the efficiency of the proposed control algorithm.
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