Bin Xu

Dr. Bin Xu

School of Automation, Northwestern Polytechnical University, Xi'an 710072, China

Research Focus & Metrics

Academic Career Length

16Years (2011-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

View All Publications
11 May 2017 in IEEE Transactions on Industrial Electronics
Verified
Journal Article
Closed access
BXBin Xu
Bin Xu
DWDanwei Wang
Danwei Wang
Youmin ZhangYoumin Zhang
Youmin Zhang
ZSZhongke Shi
Zhongke Shi
This paper investigates the disturbance observer (DOB)-based neural adaptive control on the longitudinal dynamics of a flexible hypersonic flight vehicle (HFV) in the presence of wind effects. The coupling effect between flexible states and rigid body, and the accessional angle of attack (AOA) due to wind, is modeled as unknown disturbance, where the nonlinear DOB is constructed using the neural approximation. For the weight update in neural networks (NNs), a novel algorithm is proposed with the additional prediction error derived from the serial-parallel estimation model (SPEM) using both neural approximation and disturbance estimation. Different from previous work, the wind effect is taken into the hypersonic flight dynamics for realistic analysis, and the novel controller is designed using compound estimation, where the NN and the DOB are constructed to deal with aerodynamic uncertainty and unknown disturbance. Simulation studies of a flexible HFV with wind effects show that the proposed controller can achieve high tracking accuracy, while the compound estimation can closely follow the system uncertainty with fast convergence.


14 March 2013 in Asian Journal of Control
Verified
Journal Article
Closed access
PDF file
BXBin Xu
Bin Xu
XHXiyuan Huang
Xiyuan Huang
DWDanwei Wang
Danwei Wang
FSFuchun Sun
Fuchun Sun

19 February 2018 in IEEE Transactions on Cybernetics
Verified
Journal Article
Closed access
BXBin Xu
Bin Xu
ZSZhongke Shi
Zhongke Shi
FSFuchun Sun
Fuchun Sun
WHWei He
Wei He
This paper investigates a fault-tolerant control of the hypersonic flight vehicle using back-stepping and composite learning. With consideration of angle of attack (AOA) constraint caused by scramjet, the control laws are designed based on barrier Lyapunov function. To deal with the unknown actuator faults, a robust adaptive allocation law is proposed to provide the compensation. Meanwhile, to obtain good system uncertainty approximation, the composite learning is proposed for the update of neural weights by constructing the serial-parallel estimation model to obtain the prediction error which can dynamically indicate how the intelligent approximation is working. Simulation results show that the controller obtains good system tracking performance in the presence of AOA constraint and actuator faults.

9 March 2015 in Science China Information Sciences
Verified
Journal Article
Closed access
PDF file
BXBin Xu
Bin Xu
ZSZhongKe Shi
ZhongKe Shi

31 January 2017 in IEEE Transactions on Cybernetics
Verified
Journal Article
Closed access
BXBin Xu
Bin Xu
FSFuchun Sun
Fuchun Sun
This paper addresses the dynamic surface control of uncertain nonlinear systems on the basis of composite intelligent learning and disturbance observer in presence of unknown system nonlinearity and time-varying disturbance. The serial-parallel estimation model with intelligent approximation and disturbance estimation is built to obtain the prediction error and in this way the composite law for weights updating is constructed. The nonlinear disturbance observer is developed using intelligent approximation information while the disturbance estimation is guaranteed to converge to a bounded compact set. The highlight is that different from previous work directly toward asymptotic stability, the transparency of the intelligent approximation and disturbance estimation is included in the control scheme. The uniformly ultimate boundedness stability is analyzed via Lyapunov method. Through simulation verification, the composite intelligent learning with disturbance observer can efficiently estimate the effect caused by system nonlinearity and disturbance while the proposed approach obtains better performance with higher accuracy.