TY - JOUR
T1 - Distributed Finite-Time Fault-Tolerant Containment Control for Multiple Unmanned Aerial Vehicles
AU - Yu, Ziquan
AU - Liu, Zhixiang
AU - Zhang, Youmin
AU - Qu, Yaohong
AU - Su, Chun Yi
N1 - Publisher Copyright:
© 2012 IEEE.
PY - 2020/6
Y1 - 2020/6
N2 - This paper investigates the distributed finite-time fault-tolerant containment control problem for multiple unmanned aerial vehicles (multi-UAVs) in the presence of actuator faults and input saturation. The distributed finite-time sliding-mode observer (SMO) is first developed to estimate the reference for each follower UAV. Then, based on the estimated knowledge, the distributed finite-time fault-tolerant controller is recursively designed to guide all follower UAVs into the convex hull spanned by the trajectories of leader UAVs with the help of a new set of error variables. Moreover, the unknown nonlinearities inherent in the multi-UAVs system, computational burden, and input saturation are simultaneously handled by utilizing neural network (NN), minimum parameter learning of NN (MPLNN), first-order sliding-mode differentiator (FOSMD) techniques, and a group of auxiliary systems. Furthermore, the graph theory and Lyapunov stability analysis methods are adopted to guarantee that all follower UAVs can converge to the convex hull spanned by the leader UAVs even in the event of actuator faults. Finally, extensive comparative simulations have been conducted to demonstrate the effectiveness of the proposed control scheme.
AB - This paper investigates the distributed finite-time fault-tolerant containment control problem for multiple unmanned aerial vehicles (multi-UAVs) in the presence of actuator faults and input saturation. The distributed finite-time sliding-mode observer (SMO) is first developed to estimate the reference for each follower UAV. Then, based on the estimated knowledge, the distributed finite-time fault-tolerant controller is recursively designed to guide all follower UAVs into the convex hull spanned by the trajectories of leader UAVs with the help of a new set of error variables. Moreover, the unknown nonlinearities inherent in the multi-UAVs system, computational burden, and input saturation are simultaneously handled by utilizing neural network (NN), minimum parameter learning of NN (MPLNN), first-order sliding-mode differentiator (FOSMD) techniques, and a group of auxiliary systems. Furthermore, the graph theory and Lyapunov stability analysis methods are adopted to guarantee that all follower UAVs can converge to the convex hull spanned by the leader UAVs even in the event of actuator faults. Finally, extensive comparative simulations have been conducted to demonstrate the effectiveness of the proposed control scheme.
KW - Distributed fault-tolerant containment control
KW - finite-time control
KW - input saturation
KW - neural networks (NNs)
KW - unmanned aerial vehicles (UAVs)
UR - https://www.scopus.com/pages/publications/85076239323
U2 - 10.1109/TNNLS.2019.2927887
DO - 10.1109/TNNLS.2019.2927887
M3 - 文章
C2 - 31403444
AN - SCOPUS:85076239323
SN - 2162-237X
VL - 31
SP - 2077
EP - 2091
JO - IEEE Transactions on Neural Networks and Learning Systems
JF - IEEE Transactions on Neural Networks and Learning Systems
IS - 6
M1 - 8793238
ER -