个人简介
桂海潮，现为北京航空航天大学宇航学院航天飞行器技术系教授，博士生导师，航天动力学与智能控制实验室核心成员。担任中国宇航学会空间科学与试验专委会委员，中国空间科学学会青年委员。担任英国机械工程师协会主办的期刊 IMechE Part G: Journal of Aerospace Engineering的编委。
2009年7月和2014年7月在北京航空航天大学分别获学士和博士学位，指导教师为徐世杰教授。2014年7月-2016年7月，在加拿大约克大学地球空间科学与工程系从事博士后研究，研究复杂航天器的姿态轨道一体化控制技术，合作导师为George Vukovich教授。2016年7月至2017年8月，在加拿大瑞尔森大学航空航天工程系从事博士后研究，研究小天体探测和航天器运动高精度估计技术，合作导师为Anton de Ruiter教授。2017年9月入选北航“卓越百人”青年人才引进计划，进入北航宇航学院从事教学科研工作。2017年12月入选北航“青年拔尖人才支持计划”。
主讲研究生学科理论核心课《非线性控制理论》（32学时）、本科生通识课《深空探测导论》（32学时，与王悦老师共同主讲）。指导本科生毕业设计论文荣获“2019年北京市普通本科高校优秀本科生毕业设计”、教育部“首届全国高等学校航空航天类专业本科毕业设计大赛”二等奖、三等奖，指导本科生获冯如杯科技制作竞赛二等奖、三等奖多项。
主要研究兴趣为航天器动力学、制导导航与控制技术。发表学术论文50余篇，其中SCI索引论文30余篇，相继刊登在航天动力学与控制领域的著名期刊如Journal of Guidance, Control, and Dynamics、Automatica、IEEE TAC、IEEE TCST等。获国家发明专利2项。主持科研项目十余项，包括国家自然科学基金（青年项目、面上项目）、装备预研基金、国家重点实验室基金、航天院所合作课题、商业航天课题等。
教育经历
2009.9 -- 2014.7 北京航空航天大学 航空宇航科学与技术 博士研究生毕业 博士学位 飞行器设计
2005.9 -- 2009.7 北京航空航天大学 航空宇航科学与技术 大学本科毕业 学士学位 飞行器设计与工程（航天）
工作经历
2021.12 -- 至今 北京航空航天大学 宇航学院 教授，博士生导师
2017.9 -- 2021.11 北京航空航天大学 宇航学院 副教授，博士生导师（2018.07） China
2016.7 -- 2017.8 Ryerson University(现名 Toronto Metropolitan University) Department of Aerospace Engineering 博士后研究员
2014.7 -- 2016.7 York University Department of Earth and Space Science and Engineering 博士后研究员
社会兼职
2022.11 -- 至今 中国空间科学学会青年委员
2023.1 -- 至今 中国宇航学会空间科学与试验专业委员会 委员
2018.3 -- 至今 编委，Associate Editor, 英国机械工程师协会主办的期刊 IMechE Part G: Journal of Aerospace Engineering
2018.5 -- 2018.5 Co-chair for “Space structures of tethers”, 4th IAA Conference on Dynamics and Control of Space Systems, Changsha, China, 21 May-23 May, 2018
二十余个控制和航天领域的著名期刊和会议的审稿专家，包括Automatica, Journal of Guidance, Control, and Dynamics, IEEE Transactions on Automatic Control, IEEE Transactions on Industrial Electronics, IEEE/ASME Transactions on Mechatronics, IEEE Transactions on Systems, Man and Cybernetics; IEEE Transactions on Control Systems Technology; IEEE Transactions on Aerospace and Electronic Systems； IMechE Part G: Journal of Aerospace Engineering; Acta Astronautica; Aerospace Science and Technology; Journal of Aerospace Engineering等
近期论文
查看导师新发文章
（温馨提示：请注意重名现象，建议点开原文通过作者单位确认）
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]
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]
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]
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
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
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
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
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
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
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
党庆庆，桂海潮*，徐明，徐世杰. 无速度反馈的航天器姿轨耦合跟踪控制[J]. 航空学报（增刊），1-11，2018
H. Gui, A. H. J. de Ruiter*, “Control of Asteroid-Hovering Spacecraft with Disturbance Rejection Using Position-Only Measurements,” Journal of Guidance, Control, and Dynamics, 2017, 40(10): 2401-2416
H. Gui*, G. Vukovich, “Robust Switching of Modified Rodrigues Parameter Sets for Saturated Global Attitude Control,” Journal of Guidance, Control, and Dynamics, 2017, 40(6): 1529-1542
H. Gui*, G. Vukovich, “Comments on ‘Finite-Time Consensus and Collision Avoidance Control Algorithms for Multiple AUVs’ [Automatica, 2013, 49(11), 3359–3367],” Automatica, 2017, 75: 75–76
H. Gui*, G. Vukovich, “Adaptive Fault-Tolerant Spacecraft Attitude Control Using A Novel Integral Terminal Sliding Mode,” International Journal of Robust and Nonlinear Control, 2017; 27: 3174–3196
H. Gui, G. Vukovich*, “Finite-Time Angular Velocity Observers for Rigid-Body Attitude Tracking with Bounded Inputs,” International Journal of Robust and Nonlinear Control, 2017, 27:15–38
G. Vukovich*, H. Gui, “Robust Adaptive Tracking of Rigid-Body Motion with Applications to Asteroid Proximity Operations,” IEEE Transactions on Aerospace and Electronic Systems, 2017, 53(1): 419-430
D. Lee*, G. Vukovich, H. Gui, “Adaptive Variable-Structure Finite-Time Control for Spacecraft Proximity Operations with Actuator Saturation,” Advances in Space Research, 2017, 59: 2473–2487
H. Gui, G. Vukovich*, “Finite-Time Output-Feedback Position and Attitude Tracking of a Rigid Body,” Automatica, 2016, 74: 270–278
H. Gui*, G. Vukovich, “Global Finite-Time Attitude Tracking via Quaternion Feedback,” Systems and Control Letters, 2016, 97: 176–183
H. Gui*, G. Vukovich, S. Xu, “Attitude Stabilization of a Spacecraft with Two Parallel Control Moment Gyros,” Journal of Guidance, Control, and Dynamics, 2016, 39(3): 724-731
H. Gui, G. Vukovich*, “Dual-Quaternion-Based Adaptive Motion Tracking of Spacecraft with Reduced Control Effort,” Nonlinear Dynamics, 2016, 83(1-2):597-614
H. Gui*, L. Jin, S. Xu, “Small-Time Local Controllability of Spacecraft Attitude Using Control Moment Gyros,” Automatica, 2015, 51(3): 141-148
H. Gui*, G. Vukovich, S. Xu, “Attitude Tracking of a Rigid Spacecraft Using Two Internal Torques,” IEEE Transactions on Aerospace and Electronic Systems, 2015, 51(4): 2900-2913
H. Gui*, L. Jin, S. Xu, J. Zhang, “On the Attitude Stabilization of a Rigid Spacecraft by Two Skew Control Moment Gyros,” Nonlinear Dynamics, 2015, 79(3): 2079-2097
H. Gui, L. Jin*, S. Xu, “Simple Finite-Time Attitude Stabilization Laws for Rigid Spacecraft with Bounded Inputs,” Aerospace Science and Technology, 2015, 42: 176-186
H. Gui, G. Vukovich*, “Adaptive Integral Sliding Mode Control for Spacecraft Attitude Tracking with Actuator Uncertainty,” Journal of the Franklin Institute, 2015, 352(12): 5832–5852
H. Gui, G. Vukovich*, “Robust Adaptive Spin-axis Stabilization of a Symmetric Spacecraft Using Two Bounded Torques,” Advances in Space Research, 2015, 56(11): 2495–2507
H. Gui, L. Jin*, S. Xu, “Maneuver Planning of a Rigid Spacecraft with Two Skew Control Moment Gyros,” Acta Astronautica, 2014, 104(1): 293-303
桂海潮*，徐世杰，金磊. 基于动态逆法的欠驱动航天器姿态机动控制[J]. 中国空间科学技术, 2014, 34(1): 1-9
H. Gui, L. Jin*, S. Xu, “Attitude Maneuver Control of a Two-Wheeled Spacecraft with Bounded Wheel Speeds,” Acta Astronautica, 2013, 88: 98-107
H. Gui, L. Jin*, S. Xu, “Local Controllability and Stabilization of Spacecraft Attitude by Two Single-Gimbal Control Moment Gyros,” Chinese Journal of Aeronautics, 2013, 26(5): 1218-1226
H. Gui, L. Jin*, S. Xu, “Attitude Control of a Rigid Spacecraft with One Variable-Speed Control Moment Gyro,” Acta Mechanica Sinica, 2013, 29(5): 749-760
桂海潮*, 徐世杰, 金磊, 张军. 轮控欠驱动航天器的姿态控制特性分析[J]. 中国空间科学技术, 32(5): 27-33, 2012
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