桂海潮
职称\职位:特别副研究员\博士生导师
出生年月:1986年11月
电子邮箱:hcgui@buaa.edu.cn 办公地点:北航新主楼B座1025
办公电话:



基本情况


教育背景：
2009.09-2014.06，北京航空航天大学，宇航学院，飞行器设计专业，硕博连读，获博士学位；
2005.09-2009.06，北京航空航天大学，宇航学院，飞行器设计与工程(航天)专业，学士学位。
工作经历：
2017.09-至今，北京航空航天大学，宇航学院，“卓越百人”特别副研究员，硕士生导师；
2016.07-2017.08，加拿大瑞尔森大学，航空航天工程系，博士后；
2014.07-2016.07，加拿大约克大学，地球与空间科学工程系，博士后；



研究方向


主要从事航天动力学、制导导航与控制方面的研究，具体的研究兴趣有
1.航天器姿态、姿轨耦合动力学与控制
2.编队航天器的协同控制
3.姿态确定，航天器相对运动状态估计
4.欠驱动航天器的姿态控制
5.执行机构操纵律，新型姿态控制机构


科研成果




当前主持国家自然科学基金青年基金项目1项，参与国家自然科学基金重点项目1项。曾经参与加拿大NSERC基金项目3项，973课题1项，国家自然科学基金1项。

发表学术论文30余篇，其中SCI检索20余篇，论文发表在控制理论和航天领域的重要期刊如《Automatica》、《Systems & Control Letters》、《AIAA Journal of Guidance, Control, and Dynamics》等，代表性论文如下：


期刊论文
［1］ 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
［2］ H. Gui, G. Vukovich, “Finite-Time Output-Feedback Position and Attitude Tracking of a Rigid Body,” Automatica, 2016, 74: 270–278
［3］ H. Gui, L. Jin, S. Xu, “Small-Time Local Controllability of Spacecraft Attitude Using Control Moment Gyros,” Automatica, 2015, 51(3): 141-148
［4］ 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
［5］ H. Gui, A. H. J. de Ruiter, “Adaptive Fault-Tolerant Spacecraft Pose Tracking with Control Allocation,” IEEE Transactions on Control Systems Technology, published online, 2018
［6］ H. Gui, G. Vukovich, “Global Finite-Time Attitude Tracking via Quaternion Feedback,” Systems & Control Letters, 2016, 97: 176–183
［7］ H. Gui, A. H. J. de Ruiter, “Robustness Analysis and Performance Tuning for the Quaternion Proportional–Derivative Attitude Controller,” Journal of Guidance, Control, and Dynamics, published online, 2018
［8］ H. Gui, A. H. J. de Ruiter, “Quaternion Invariant Extended Kalman Filtering for Spacecraft Attitude Estimation,” AIAA Journal of Guidance, Control, and Dynamics, 2018, 41(4): 863–878
［9］ H. Gui, A. H. J. de Ruiter, “Control of Spacecraft Hovering About Asteroids Using Position-Only Measurements,” AIAA Journal of Guidance, Control, and Dynamics, 2017, 40(10): 2401-2416
［10］ H. Gui, G. Vukovich, “Robust Switching of Two Modified Rodrigues Parameter Sets for Saturated Global Attitude Control,” AIAA Journal of Guidance, Control, and Dynamics, 2017, 40(6): 1529-1542
［11］ H. Gui, G. Vukovich, S. Xu, “Attitude Stabilization of a Spacecraft with Two Parallel Control Moment Gyros,” AIAA Journal of Guidance, Control, and Dynamics, 2016, 39(3): 724-731
［12］ 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
［13］ 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
［14］ 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
［15］ 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
［16］ H. Gui, G. Vukovich, “Dual-Quaternion-Based Adaptive Motion Tracking of Spacecraft with Reduced Control Effort,” Nonlinear Dynamics, 2016, 83:597-614
［17］ 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
［18］ H. Gui, G. Vukovich, “Adaptive Integral Sliding Mode Control for Spacecraft Attitude Tracking with Actuator Uncertainty,” Journal of the Franklin Institute-Engineering and Applied Mathematics, 2015, 352(12): 5832-5852
［19］ 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
［20］ 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
［21］ H. Gui, L. Jin, S. Xu, “Attitude Maneuver Control of a Two-Wheeled Spacecraft with Bounded Wheel Speeds,” Acta Astronautica, 2013, 88: 98-107
［22］ 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
［23］ 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
［24］ 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
［25］ 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
［26］ 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(10): 2473-2487




主要奖励：


2015年北京航空航天大学优秀博士论文