Yiwei Xu
10 Papers
Yiwei Xu is an academic researcher. The author has contributed to research in topics: Computer science & Control theory (sociology). The author has an hindex of 1, co-authored 9 publications.
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Papers
Fractional‐order fault‐tolerant containment control of multiple fixed‐wing UAVs via disturbance observer and interval type‐2 fuzzy neural network
TL;DR: In this article , a fractional-order containment control (FTCC) scheme is established to steer all follower UAVs into the convex hull formed by the leader UAV with the involvements of FO calculus, disturbance observers (DOs), and interval type-2 fuzzy neural networks (IT2FNNs).
10
Research on preprocessing of winding trajectory of composite type IV pressure vessel based on robot
TL;DR: In this article , a smooth preprocessing method of robotic end-effector trajectory, based on Nurbs curve, is proposed for obtaining the complete and stable envelope trajectory of the robot.
2
Fractional-Order Sliding-Mode Fault-Tolerant Control of Unmanned Airship Against Actuator Faults
TL;DR: In this article , a fractional-order sliding-mode fault-tolerant control scheme for unmanned airships in the presence of actuator faults is proposed, where a control-oriented unmanned airship model is first developed by considering the unexpected actuator failures.
2
Signal Fingerprint-Based Identification for Multi-rotor UAV Remote Control Terminal
Xuetao Zhang,Kuangang Fan,Yiwei Xu,Bing He,Wengang Tan +4 more
- 16 Dec 2022
TL;DR: Wang et al. as mentioned in this paper proposed two fingerprint-based methods for identifying different remote controllers of UAVs and compared the two identification methods with five machine learning methods, such as decision tree(Tree), Naive Bayes (NB), Discriminant analysis (Discr), k-nearest neighbor (KNN) and Error Correction Output Coding (ECOC).
1
Adaptive Neural Network Finite-Time Fault-Tolerant Control of Fixed-Wing UAV Under State Constraints and Actuator Fault
Yiwei Xu,Zhong Yang,Ruifeng Zhou,Ziquan Yu,Fu Yang Chen,Youmin Zhang +5 more
- 24 Aug 2022
TL;DR: In this paper , an adaptive neural network finite-time fault-tolerant control scheme is proposed for a fixed-wing UAV under state constraints and actuator fault, which can solve the algebraic loop involved by control input.