Profile

【基本情况】
桂明臻，男，博士，江西南昌人，中南大学自动化学院副教授。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。主要研究方向：（1）航天器自主导航方法；（2）深空探测器新型智能导航方法；（3）非线性自适应最优估计方法。主持和参与了国家自然科学基金青年项目、湖南省自然科学基金青年项目、航天一院高校联合创新基金项目、航天五院合作项目、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、IEEE Transactions on Instrumentation and Measurement、Aerospace Science and Technology等期刊发表SCI论文二十余篇，授权国家发明专利十余项。受邀担任广东省自然科学基金评审专家、《深空探测学报（中英文）》青年编委、SCI期刊Applied Sciences(IF: 2.7)客座主编、Frontiers in Aerospace Engineering Review Editor、湖南省信息技术标准化技术委员会专家，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。

----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------

硕士研究生招生专业方向：控制科学与工程，电子信息工程，1-3人/年

本科专业不限，不要求学生本科掌握导航相关知识，有能力、有信心让零基础学生快速入门。

鼓励学生产出成果，并给予优厚助研金及成果奖励，支持学生申报各种荣誉奖励，

目前所带研究生人均产出论文3篇，获中南大学2024届优秀毕业生、华为校级奖学金，热忱欢迎对航天及导航感兴趣的有志青年加入！

【代表论著】

[1] Gui Mingzhen, Yang Hua, et al. A Novel Sun Direction/Solar Disk Velocity Difference Integrated Navigation Method Against Installation Error of Spectrometer Array[J]. IEEE Sensors Journal. 2023, doi: 10.1109/JSEN.2023.3288540.(Q1)

[2] Gui Mingzhen, Yang Hua, et al. Variational Bayesian implicit unscented Kalman filter for celestial navigation using time delay measurement[J]. Advances in Space Research. 2023, 71(1): 756-767.(Q1)

[3] Gui Mingzhen, Yang Hua, et al. Star angle/ double-differenced pulse time of arrival integrated navigation method for Jupiter exploration[J]. Advances in Space Research. 2023, 71(6): 2669-2678.(Q1)

[4] Gui Mingzhen, Yang Hua, et al. Parameter-Independent Event-Triggered Implicit UKF for the Celestial Navigation Using Time Delay Measurement[J]. Mathematics. 2023, 11(8): 1-14.(Q1)

[5] Gui Mingzhen, Wei Caisheng, et al. Analysis and Compensation of Sun Direction Error on Solar Disk Velocity Difference [J]. Mathematics, 2023, 11(17): 1-14.(Q1)

[6] Gui Mingzhen, Zhao Dangjun, et al. A Time Delay/ Star Angle Integrated Navigation Method Based on the Event-triggered Implicit Unscented Kalman Filter[J]. IEEE Transactions on Instrumentation and Measurement. 2021, 70: 1-10.(Q1)

[7] 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.(Q1)

[8] 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.(Q1)

[9] 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.(Q1)

[10] 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.(Q1)

[11] 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.(Q1)

[12] Ning Xiaolin, Gui Mingzhen, et al. INS/VNS/CNS integrated navigation method for planetary rovers[J]. Aerospace Science and Technology, 2016, 48: 102-14.(Q1)

[13] Ning Xiaolin, Gui Mingzhen, et al. Solar oscillation time delay measurement assisted celestial navigation method[J]. Acta Astronautica, 2017, 134: 152-8.(Q1)

[14] 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.(Q1)

[15] 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.(Q1)

[16] 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.(Q1)

[17] 桂明臻, 魏一丰等, 考虑相对论效应的火星探测器天文测角导航 [J]. 深空探测学报(中英文), 2023, 10(02): 126-32.

[18] 桂明臻, 宁晓琳等, 一种快速星光角距/时间延迟量测组合导航方法[J]. 深空探测学报(中英文), 2021, 8(02): 190-7.

[19] 桂明臻, 宁晓琳等, 考虑星历误差的天文测角/时间延迟量测组合导航方法[J]. 飞控与探测, 2020, 3(04): 24-32.

[20] 宁晓琳, 桂明臻等, 基于TOA和TDTOA的增广状态脉冲星组合导航误差抑制方法[J]. 中国科学:信息科学, 2021, 51(06): 971-84.

[1] 航天器自主导航方法

[2] 深空探测器新型智能导航方法

[3] 非线性自适应最优估计方法

[1]   广东省自然科学基金评审专家

[2]   《深空探测学报（中英文）》青年编委

[3]   Applied Sciences(IF: 2.7)客座主编

[4]   Frontiers in Aerospace Engineering Review Editor

[5]   湖南省信息技术标准化技术委员会专家

[6]   IEEE Member、中国自动化学会会员、中国宇航学会会员、湖南省宇航学会会员

[7]   IEEE Transactions on Aerospace and Electronic Systems、IEEE Access、AA、JON、JAE、ASR等SCI期刊审稿人

[1]  2013.9- 2019.6

北京航空航天大学 | PhD Graduate | Doctoral degree

[2]  2009.9- 2013.6

西北工业大学 | University graduated | Bachelor's degree

 Email:3876d9fca88b803777153fba7db80af444708937c331a8b45ecdea9e56bad2953c60a3ff5b6d01cce33ba476f9e4b3c3a760f9382020151d80afc5287efbc4f80c86403cb71f071fe083c3455fcc44420b873ab949da446a707f6954e0e9196672b2aed8e7d4073b7cc98f0181ea8d28a891447e05ff4cd0677e142983a9f722