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 five.

Timeline

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In proceedings

Article

PhD thesis

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Bibliography

2023

Parameter Identification of a PN-Guided Incoming Missile Using an Improved Multiple-Model Mechanism.

[BibT_eX]

[DOI]

Yinhan Wang

Jiang Wang

Shipeng Fan

IEEE Trans. Aerosp. Electron. Syst., October, 2023

2022

Nonlinear Optimal 3-D Impact-Angle-Control Guidance Against Maneuvering Targets.

[BibT_eX]

[DOI]

IEEE Trans. Aerosp. Electron. Syst., 2022

Optimal Encirclement Guidance.

[BibT_eX]

[DOI]

IEEE Trans. Aerosp. Electron. Syst., 2022

Generalized Control Coupling Effect of Spinning Guided Projectiles.

[BibT_eX]

[DOI]

Shipeng Fan

Jiang Wang

Defu Lin

IEEE Trans. Aerosp. Electron. Syst., 2022

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

[BibT_eX]

[DOI]

Shih-Yao Lin

Jiang Wang

Wei Wang

IEEE Access, 2022

2021

Optimal Guidance With Active Observability Enhancement for Scale Factor Error Estimation of Strapdown Seeker.

[BibT_eX]

[DOI]

IEEE Trans. Aerosp. Electron. Syst., 2021

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

[BibT_eX]

[DOI]

CoRR, 2021

Nonlinear Modeling the Quadcopter Considering the Aerodynamic Interaction.

[BibT_eX]

[DOI]

IEEE Access, 2021

Stability Limits for the Velocity Orientation Autopilot of Rolling Missiles.

[BibT_eX]

[DOI]

IEEE Access, 2021

2019

Integral Global Sliding Mode Guidance for Impact Angle Control.

[BibT_eX]

[DOI]

Shaoming He

Defu Lin

Jiang Wang

IEEE Trans. Aerosp. Electron. Syst., 2019

2017

A novel sliding mode guidance law without line-of-sight angular rate information accounting for autopilot lag.

[BibT_eX]

[DOI]

Shaoming He

Jiang Wang

Wei Wang

Int. J. Syst. Sci., 2017

2016

Optimal integral sliding mode guidance law based on generalized model predictive control.

[BibT_eX]

[DOI]

Jiang Wang

Shaoming He

J. Syst. Control. Eng., 2016

Three-dimensional multivariable integrated guidance and control design for maneuvering targets interception.

[BibT_eX]

[DOI]

Shaoming He

Wei Wang

Jiang Wang

J. Frankl. Inst., 2016

Disturbance observer-based robust integrated guidance and control design for tactical missiles.

[BibT_eX]

[DOI]

Proceedings of the 12th IEEE International Conference on Control and Automation, 2016

2015

Autonomous spacecraft rendezvous with finite time convergence.

[BibT_eX]

[DOI]

Shaoming He

Defu Lin

Jiang Wang

J. Frankl. Inst., 2015

Jiang Wang

Timeline

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