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桂海潮 ( 教授 ) 赞
的个人主页 http://shi.buaa.edu.cn/guihaichao/zh_CN/index.htm
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[1] .H. Gui, “Observer-Based Fault-Tolerant Spacecraft Attitude Tracking Using Sequential Lyapunov Analyses,” IEEE Transactions on Automatic Control, 2021, 66(12): 6108-6114.[期刊]
[2] .H. Gui*, Y. Wang, W. Su, “Hybrid Global Finite-Time Dual-Quaternion Observer and Controller for Velocity-Free Spacecraft Pose Tracking,” IEEE Transactions on Control Systems Technology, 2021, 29(5):2129-2141.[期刊]
[3] .Q. Dang, H. Gui, K. Liu*, “Relaxed-Constraint Pinpoint Lunar Landing Using Geometric Mechanics and Model Predictive Control,” Journal of Guidance, Control, and Dynamics, 2020, 43(9): 1617-1630.[期刊]
[4] .Q. Dang, H. Gui*, H. Wen, “Dual-Duaternion-Based Spacecraft Pose Tracking With a Global Exponential Velocity Observer,” Journal of Guidance, Control, and Dynamics, 2019, 42(9): 2106–2115
[5] .Q. Dang, H. Gui*, M. Xu, H. Wen, “Dual-Quaternion Immersion and Invariance Velocity Observer for Controlling Asteroid-Hovering Spacecraft,” Acta Astronautica, 2019, 16: 304-312
[6] .H. Gui*, A. H. J. de Ruiter, “Adaptive Fault-Tolerant Spacecraft Pose Tracking with Control Allocation,” IEEE Transactions on Control Systems Technology, 2019, 27(2):479-494
[7] .H. Gui*, A. H. J. de Ruiter, “Robustness Analysis and Performance Tuning for the Quaternion PD+ Attitude Controller,” Journal of Guidance, Control, and Dynamics, 2018, 41(10): 2305-2314
[8] .H. Gui*, A. H. J. de Ruiter, “Global Finite-Time Attitude Consensus of Leader-Following Spacecraft Systems Based on Distributed Observers,” Automatica, 2018, 91: 225~232
[9] .H. Gui, A. H. J. de Ruiter*, “Quaternion Invariant Extended Kalman Filtering for Spacecraft Attitude Estimation,” Journal of Guidance, Control, and Dynamics, 2018, 41(4): 863–878
[10] .H. Gui*, G. Vukovich, “Distributed Almost Global Finite-Time Attitude Consensus of Multiple Spacecraft Without Velocity Measurements,” Aerospace Science and Technology, 2018, 75: 284–296

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