Jiang Wang

Orcid: 0000-0002-2754-6471

Affiliations:
  • Beijing Institute of Technology, School of Aerospace Engineering, China (PhD 2008)


According to our database1, Jiang Wang authored at least 15 papers between 2015 and 2023.

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

Timeline

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Bibliography

2023
Parameter Identification of a PN-Guided Incoming Missile Using an Improved Multiple-Model Mechanism.
IEEE Trans. Aerosp. Electron. Syst., October, 2023

2022
Nonlinear Optimal 3-D Impact-Angle-Control Guidance Against Maneuvering Targets.
IEEE Trans. Aerosp. Electron. Syst., 2022

Optimal Encirclement Guidance.
IEEE Trans. Aerosp. Electron. Syst., 2022

Generalized Control Coupling Effect of Spinning Guided Projectiles.
IEEE Trans. Aerosp. Electron. Syst., 2022

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

2021
Optimal Guidance With Active Observability Enhancement for Scale Factor Error Estimation of Strapdown Seeker.
IEEE Trans. Aerosp. Electron. Syst., 2021

Computational Impact Time Guidance: A Learning-Based Prediction-Correction Approach.
CoRR, 2021

Nonlinear Modeling the Quadcopter Considering the Aerodynamic Interaction.
IEEE Access, 2021

Stability Limits for the Velocity Orientation Autopilot of Rolling Missiles.
IEEE Access, 2021

2019
Integral Global Sliding Mode Guidance for Impact Angle Control.
IEEE Trans. Aerosp. Electron. Syst., 2019

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

2016
Optimal integral sliding mode guidance law based on generalized model predictive control.
J. Syst. Control. Eng., 2016

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

Disturbance observer-based robust integrated guidance and control design for tactical missiles.
Proceedings of the 12th IEEE International Conference on Control and Automation, 2016

2015
Autonomous spacecraft rendezvous with finite time convergence.
J. Frankl. Inst., 2015


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