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Shengjing Tang
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2020 – today
- 2022
- [j7]Ziyao Wang
, Shengjing Tang
Entry Guidance Command Generation for Hypersonic Glide Vehicles Under Threats and Multiple Constraints. IEEE Access 10: 1-15 (2022) - [j6]Jiali Li
Noise-Adaption Extended Kalman Filter Based on Deep Deterministic Policy Gradient for Maneuvering Targets. Sensors 22(14): 5389 (2022) - 2020
- [j5]Huixin Zheng
Smooth Sub-Optimal Trajectory Generation for Transition Maneuvers. IEEE Access 8: 61035-61042 (2020)
2010 – 2019
- 2019
- [j4]Haichao Hong
Adaptive trajectory generation based on real-time estimated parameters for impaired aircraft landing. Int. J. Syst. Sci. 50(15): 2733-2751 (2019) - [j3]Haichao Hong
Model Predictive Convex Programming for Constrained Vehicle Guidance. IEEE Trans. Aerosp. Electron. Syst. 55(5): 2487-2500 (2019) - [j2]Yulin Wang
Fuzzy-Logic-Based Fixed-Time Geometric Backstepping Control on SO(3) For Spacecraft Attitude Tracking. IEEE Trans. Aerosp. Electron. Syst. 55(6): 2938-2950 (2019) - [j1]Haichao Hong
Smooth Interpolation-Based Fixed-Final-Time Command Generation. IEEE Trans. Aerosp. Electron. Syst. 55(6): 3039-3049 (2019) - [c10]Huixin Zheng, Haichao Hong, Shengjing Tang:
An Optimal L1 Navigation Design Framework for Constrained Heading Control and Coordination. ASCC 2019: 615-620 - [c9]Xiao Wang, Yulin Wang, Shengjing Tang, Jie Guo:
Entry Trajectory Optimization via hp Pseudospectral Convex Programming. ICINCO (1) 2019: 61-69 - [c8]Yulin Wang, Xiao Wang, Shengjing Tang, Jie Guo:
Geometric Adaptive Robust Sliding-mode Control on SO(3). ICINCO (2) 2019: 328-338 - [c7]Haichao Hong
Dynamic Soaring in Unspecified Wind Shear: A Real-time Quadratic-programming Approach. MED 2019: 600-605 - 2018
- [c6]Haichao Hong
Wind Estimation for Fixed-Wing Aircraft Using Command Tracking Approach. MED 2018: 879-884 - 2012
- [c5]Jie Guo, Qian Xu, Jingnan Zhang, Shengjing Tang:
Decoupling design of rolling aircraft using adaptive neuro-fuzzy inference systems based on T-S model. FSKD 2012: 339-343 - [c4]Jie Guo, Shengjing Tang, Qian Xu:
An improved particle swarm optimization and its application in maneuvering control laws design of the unmanned aerial vehicle. ICNC 2012: 1107-1111 - 2011
- [c3]Junhui Xiong, Shengjing Tang, Jie Guo:
Approach of aircraft configuration with complex free-form surface design based on reverse engineering. EMEIT 2011: 2757-2761
2000 – 2009
- 2009
- [c2]Jie Guo, Shengjing Tang:
Application of Parameter Self-Tuning Fuzzy PID Controller in Guidance Loop of Unmanned Aircraft. FSKD (4) 2009: 57-61 - 2007
- [c1]Rui Xu, Huiping Jiang, Shengjing Tang, Pingyuan Cui, Fuzhan Yue:
Analyzing and designing of lunar rover motion controller. ROBIO 2007: 1574-1579
Coauthor Index
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