Wei Wang

Orcid: 0000-0002-6941-2236

Affiliations:
  • Beijing Institute of Technology, School of Aerospace Engineering, China


According to our database1, Wei Wang authored at least 13 papers between 2016 and 2023.

Collaborative distances:
  • Dijkstra number2 of five.
  • Erdős number3 of four.

Timeline

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Bibliography

2023
Piecewise Trajectory and Angle Constraint-Based Fractional-Order Sliding Mode Control.
IEEE Trans. Aerosp. Electron. Syst., October, 2023

Accurate Ovarian Cyst Classification With a Lightweight Deep Learning Model for Ultrasound Images.
IEEE Access, 2023

2022
Nonlinear Guidance Laws for Maneuvering Target Interception With Virtual Look Angle Constraint.
IEEE Trans. Aerosp. Electron. Syst., 2022

Nonlinear modified bias proportional navigation guidance law against maneuvering targets.
J. Frankl. Inst., 2022

Barrier Lyapunov Function Based Integrated Missile Guidance and Control Considering Phased Array Seeker Disturbance Rejection Rate.
IEEE Access, 2022

2021
Online Reentry Trajectory Optimization Using Modified Sequential Convex Programming for Hypersonic Vehicle.
IEEE Access, 2021

2020
Velocity-Free Fault-Tolerant Rendezvous Law Based on Dual-Layer Adaptive Algorithm.
IEEE Access, 2020

2019
A novel approximate finite-time convergent guidance law with actuator fault.
Clust. Comput., 2019

A Novel Online Estimation and Compensation Method for Strapdown Phased Array Seeker Disturbance Rejection Effect Using Extended State Kalman Filter.
IEEE Access, 2019

2018
Consensus-Based Two-Stage Salvo Attack Guidance.
IEEE Trans. Aerosp. Electron. Syst., 2018

2017
A novel sliding mode guidance law without line-of-sight angular rate information accounting for autopilot lag.
Int. J. Syst. Sci., 2017

2016
Robust output feedback control design for autonomous spacecraft rendezvous with actuator faults.
J. Syst. Control. Eng., 2016

Three-dimensional multivariable integrated guidance and control design for maneuvering targets interception.
J. Frankl. Inst., 2016


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