Autonomous spacecraft rendezvous with finite time convergence. - Shaoming He; Defu Lin; Jiang Wang 006 (J. Frankl. Inst., 2015)

Disturbance observer-based robust integrated guidance and control design for tactical missiles. - Shaoming He; Tao Song 004; Jiang Wang 006; Defu Lin (ICCA, 2016)

Three-dimensional multivariable integrated guidance and control design for maneuvering targets interception. - Shaoming He; Wei Wang 218; Jiang Wang 006 (J. Frankl. Inst., 2016)

Optimal integral sliding mode guidance law based on generalized model predictive control. - Jiang Wang 006; Shaoming He (J. Syst. Control. Eng., 2016)

A novel sliding mode guidance law without line-of-sight angular rate information accounting for autopilot lag. - Shaoming He; Jiang Wang 006; Wei Wang 218 (Int. J. Syst. Sci., 2017)

Integral Global Sliding Mode Guidance for Impact Angle Control. - Shaoming He; Defu Lin; Jiang Wang 006 (IEEE Trans. Aerosp. Electron. Syst., 2019)

Stability Limits for the Velocity Orientation Autopilot of Rolling Missiles. - Shaoyong Hu; Jiang Wang 006; Yuchen Wang; Song Tian (IEEE Access, 2021)

Nonlinear Modeling the Quadcopter Considering the Aerodynamic Interaction. - Jianchuan Ye; Jiang Wang 006; Tao Song 004; Zeliang Wu; Pan Tang (IEEE Access, 2021)

Computational Impact Time Guidance: A Learning-Based Prediction-Correction Approach. - Zichao Liu; Jiang Wang 006; Shaoming He; Hyo-Sang Shin; Antonios Tsourdos (CoRR, 2021)

Optimal Guidance With Active Observability Enhancement for Scale Factor Error Estimation of Strapdown Seeker. - Yadong Wang; Jiang Wang 006; Shaoming He; Hyo-Sang Shin; Antonios Tsourdos (IEEE Trans. Aerosp. Electron. Syst., 2021)

Barrier Lyapunov Function Based Integrated Missile Guidance and Control Considering Phased Array Seeker Disturbance Rejection Rate. - Shih-Yao Lin 003; Jiang Wang 006; Wei Wang 218 (IEEE Access, 2022)

Generalized Control Coupling Effect of Spinning Guided Projectiles. - Shipeng Fan; Jiang Wang 006; Defu Lin (IEEE Trans. Aerosp. Electron. Syst., 2022)

Optimal Encirclement Guidance. - Hongyan Li; Shaoming He; Jiang Wang 006; Chang-Hun Lee (IEEE Trans. Aerosp. Electron. Syst., 2022)

Nonlinear Optimal 3-D Impact-Angle-Control Guidance Against Maneuvering Targets. - Hongyan Li; Jiang Wang 006; Shaoming He; Chang-Hun Lee (IEEE Trans. Aerosp. Electron. Syst., 2022)

Parameter Identification of a PN-Guided Incoming Missile Using an Improved Multiple-Model Mechanism. - Yinhan Wang; Jiang Wang 006; Shipeng Fan (IEEE Trans. Aerosp. Electron. Syst., 2023)