Z
Ziquan Yu
Researcher at Nanjing University of Aeronautics and Astronautics
Publications - 64
Citations - 795
Ziquan Yu is an academic researcher from Nanjing University of Aeronautics and Astronautics. The author has contributed to research in topics: Computer science & Actuator. The author has an hindex of 10, co-authored 44 publications receiving 299 citations. Previous affiliations of Ziquan Yu include Concordia University Wisconsin & Concordia University.
Papers
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Distributed Fault-Tolerant Cooperative Control for Multi-UAVs Under Actuator Fault and Input Saturation
TL;DR: It is shown by Lyapunov approach and graph theory that the synchronization tracking stability can be guaranteed and all follower UAVs can track the leader UAV and the effectiveness of the proposed fault-tolerant cooperative controller is validated by numerical simulation results.
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Distributed Finite-Time Fault-Tolerant Containment Control for Multiple Unmanned Aerial Vehicles
TL;DR: 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 with extensive comparative simulations to demonstrate the effectiveness of the proposed control scheme.
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Decentralized fractional-order backstepping fault-tolerant control of multi-UAVs against actuator faults and wind effects
TL;DR: It is shown that by using Lyapunov methods the synchronization tracking control is achieved even when multi-UAVs simultaneously encounter wind effects and actuator faults.
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Decentralized finite-time adaptive fault-tolerant synchronization tracking control for multiple UAVs with prescribed performance
TL;DR: A finite-time attitude synchronization tracking control scheme is developed by using neural networks and finite- time differentiator techniques, and it is shown that by using the Lyapunov method, all UAVs can track their individual attitude references, while the synchronized tracking errors among Uavs are all bounded in finite time and confined within the prescribed performance bounds.
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Safe control of trailing UAV in close formation flight against actuator fault and wake vortex effect
TL;DR: It is shown by Lyapunov stability analysis that the closed-loop system is uniformly ultimately bounded with safety requirements guaranteed even in the presence of wake vortex and actuator faults.