桂明臻 - 中南大学 - 航空航天学院

个人简介

桂明臻，男，博士，江西南昌人，中南大学航空航天学院副教授。自2013年9月进入北京航空航天大学惯性技术国家重点实验室攻读硕士与博士学位，于2019年6月博士毕业。曾获国家奖学金、中国仪器仪表学会奖学金、北京市优秀毕业生、北航研究生十佳等奖励。主要从事深空探测器自主导航方向研究，主持和参与了国家自然科学基金青年项目、中南大学人才启动项目、国家973项目、国家自然科学基金重点项目等多个项目的研制与结题过程。在IEEE Transactions on Aerospace and Electronic Systems、Aerospace Science and Technology等期刊发表SCI论文十余篇，授权国家发明专利4项，已受理国家发明专利5项，受邀担任IEEE Transactions on Aerospace and Electronic Systems、IEEE Transactions on Industrial Informatics、IEEE Access、Acta Astronautica、Chinese Journal of Aeronautics、Journal of Navigation、Journal of Aerospace Engineering、Advances in Space Research等SCI期刊审稿人。鼓励学生产出成果，并给予优厚助研金及成果奖励，热忱欢迎有志青年加入！教育经历 [1] 2013.9-2019.6 北京航空航天大学博士学位 | 博士研究生毕业 [2] 2009.9-2013.6 西北工业大学学士学位 | 大学本科毕业工作经历 [1] 2019.9-至今中南大学 | 航空航天学院 | 特聘副教授

近期论文

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[1] Gui Mingzhen, Ning Xiaolin, et al. A Novel Celestial Aided Time-Differenced Pulsar Navigation Method Against Ephemeris Error of Jupiter for Jupiter Exploration[J]. IEEE Sensors Journal. 2019, 19(3): 1127-34. [2] Ning Xiaolin, Gui Mingzhen, et al. A Novel Autonomous Celestial Navigation Method Using Solar Oscillation Time Delay Measurement[J]. IEEE Transactions on Aerospace and Electronic Systems, 2018, 54(3): 1392-403. [3] Ning Xiaolin, Gui Mingzhen, et al. Impact of the Pulsar's Direction on CNS/XNAV Integrated Navigation[J]. IEEE Transactions on Aerospace and Electronic Systems, 2017, 53(6): 3043-55. [4] Ning Xiaolin, Gui Mingzhen, Fang Jiancheng, et al. A Novel Differential Doppler Measurement-Aided Autonomous Celestial Navigation Method for Spacecraft During Approach Phase[J]. IEEE Transactions on Aerospace and Electronic Systems, 2017, 53(2): 587-97. [5] Ning Xiaolin, Gui Mingzhen, et al. Differential X-ray pulsar aided celestial navigation for Mars exploration[J]. Aerospace Science and Technology, 2017, 62: 36-45. [6] Ning Xiaolin, Gui Mingzhen, et al. INS/VNS/CNS integrated navigation method for planetary rovers[J]. Aerospace Science and Technology, 2016, 48: 102-14. [7] Ning Xiaolin, Gui Mingzhen, et al. Solar oscillation time delay measurement assisted celestial navigation method[J]. Acta Astronautica, 2017, 134: 152-8. [8] Ning Xiaolin, Gui Mingzhen, et al. A dimension reduced INS/VNS integrated navigation method for planetary rovers[J]. Chinese Journal of Aeronautics, 2016, 29(6): 1695-708. [9] Ning Xiaolin, Zhang Jie, Gui Mingzhen, et al. A Fast Calibration Method of the Star Sensor Installation Error Based on Observability Analysis for the Tightly Coupled SINS/CNS Integrated Navigation System[J]. IEEE Sensors Journal, 2018, 18(16): 6794-803. [10] Ning Xiaolin, Yang Yuqing, Gui Mingzhen, et al. Pulsar navigation using time of arrival (TOA) and time differential TOA (TDTOA)[J]. Acta Astronautica, 2018, 142: 57-63. [11] Ning Xiaolin, Yang Yuqing, Li Zhuo, Gui Mingzhen, et al. Ephemeris Corrections in Celestial/Pulsar Navigation Using Time Differential and Ephemeris Estimation[J]. Journal of Guidance, Control, and Dynamics, 2018, 41(1): 268-75. [12] Ding Zonhe, Ning Xiaolin, Gui Mingzhen. Attitude Estimation Method for Spinning Spacecraft Using Markley Variables and Optical Flow of Stars[A]. Proceedings of the 2nd International Conference on Computer Engineering, Information Science & Application Technology[C]. 2017: 885-8 [13] Yuan Weiping, Gui Mingzhen, Ning Xiaolin. Initial Attitude Estimation and Installation Errors Calibration of the IMU for Plane by SINS/CNS Integration[A]. Proceedings of 2017 Chinese Intelligent Automation Conference[C]. 2018: 123-30 [14] Rao Yuan, Kang Zhiwei, Liu Jin, Ma Xin, Gui Mingzhen. High-accuracy pulsar time delay estimation using an FrFT-based GCC[J]. Optik, 2019, 181: 611-8 [15] Kang Zhiwei, He Hongcai, Liu Jin, Ma Xin, Gui Mingzhen. Adaptive pulsar time delay estimation using wavelet-based RLS[J]. Optik, 2018, 171: 266-76

学术兼职

[1] 受邀担任IEEE Transactions on Aerospace and Electronic Systems、IEEE Transactions on Industrial Informatics、IEEE Access、Acta Astronautica、Chinese Journal of Aeronautics、Journal of Navigation、Journal of Aerospace Engineering、Advances in Space Research等SCI期刊审稿人