基本信息科学研究教育教学English论文专著
基本信息

张刚，男，汉族，1983年生。哈尔滨工业大学卫星技术研究所教授，航空宇航科学与技术学科博士生导师。近年来一直从事飞行器轨道动力学与控制的研究工作，以第一或通讯作者身份发表和录用学术论文近40篇，包括SCI收录31篇，其中有9篇发表在航空航天顶级期刊AIAA Journal of Guidance, Control, and Dynamics上,2篇发表在航空航天顶级期刊 IEEE Transactions on Aerospace and Electronic Systems上。主持了国家自然科学基金青年和面上项目、国家863计划、博士后基金特别资助和面上项目、重点实验室开放基金等多个项目；参与了国家自然科学基金、嫦娥四号搭载探月微卫星项目、高分辨率对地观测系统重大专项、民用航天预研项目等。2016年获得航空宇航科学与技术学科全国优秀博士学位论文奖。

在参与的嫦娥四号搭载微卫星“月球轨道超长波天文观测微卫星”项目中，主要负责轨道设计与轨道控制。该卫星于2018年5月21日发射，5月25日“龙江二号”顺利进入环月轨道，成为世界上首个独立完成地月转移、近月制动、环月飞行的微卫星，哈工大也因此成为世界上首个将航天器送入月球轨道的高校。在参与的高分辨率对地观测系统重大专项“XX小卫星系统技术”项目中，主要负责多星任务规划和编队轨道控制等相关技术。

教育经历
2003.09 - 2007.07,吉林大学,数学学院信息与计算科学专业，本科2007.08 - 2012.07,哈尔滨工业大学,航天学院航空宇航科学与技术专业，博士2009.10 - 2010.10,美国Texas A&M University,航天工程系, 联合培养博士


工作经历
时间工作经历
2012.07-2015.12哈尔滨工业大学，航天学院卫星技术研究所，讲师
2016.01-2018.12哈尔滨工业大学，航天学院卫星技术研究所，（校青年拔尖）副教授
2019.01-至今哈尔滨工业大学，航空宇航科学与技术学科，（校青年拔尖）教授
2018.04-至今哈尔滨工业大学，航空宇航科学与技术学科，博士生导师



获奖与荣誉称号
2013年7月， 获哈尔滨工业大学第十五届校优秀博士学位论文奖

2016年11月，获航空宇航科学与技术学科全国优秀博士学位论文奖

2017年9月，获黑龙江省自然科学二等奖（排名第2）

2019年4月，获第十届全国空间轨道设计竞赛冠军

我的新闻
2019.04，获得第十届全国空间轨道设计竞赛冠军。链接网址

http://news.hit.edu.cn/2019/0510/c1510a216640/page.htm

2018.05，负责轨道设计与轨道控制的“龙江二号”卫星顺利进入环月轨道，成为世界上首个独立完成地月转移、近月制动、环月飞行的微卫星，哈工大也因此成为世界上首个将航天器送入月球轨道的高校。链接网址

https://heilongjiang.dbw.cn/system/2018/06/22/**.shtml

2016.11，获得航空宇航科学与技术学科全国优秀博士学位论文奖。链接网址

http://news.hit.edu.cn/2016/1116/c467a167574/page.htm


研究领域
航天器轨道动力学与控制轨道任务分析与设计主要研究方向: 轨道交会、正切轨道、小推力轨迹优化等

科研项目

项目名称面向快速响应任务的卫星星下点轨迹调整轨道机动技术研究

项目来源国家自然科学基金面上项目

开始时间2018.01

结束时间2021.12

项目经费62万

担任角色负责

项目类别纵向项目

项目状态进行中



项目名称基于正切推力的近地及火星探测轨道转移和轨道交会研究

项目来源国家自然科学基金青年基金

开始时间2015-01-01

结束时间2017-12-01

项目经费25万

担任角色负责

项目类别横向项目

项目状态完成



项目名称特定方向连续小推力轨道转移和轨道交会研究

项目来源中国博士后基金特别资助

开始时间2014-04-01

结束时间2015-12-01

项目经费15万

担任角色负责

项目类别纵向项目

项目状态完成



项目名称基于XX参数补偿的XX轨道预报技术

项目来源国家863计划

开始时间2015-10-01

结束时间2016-06-01

项目经费60

担任角色负责

项目类别横向项目

项目状态完成


讲授课程
目前讲授本科生选修课程《飞行器轨道动力学中的数学方法》

简介:飞行器轨道动力学是轨道任务设计的基础，本课程将在轨道力学经典书籍《An Introduction to the Mathematics and Methods of Astrodynamics》 (Battin R.H.著，1999年)的基础上，讲解航天器轨道动力学中的基本问题和基本数学方法，并应用于轨道转移和轨道交会等任务。培养本科生在所学轨道动力学基础知识上，掌握轨道动力学领域所需的基本数学方法，并用于轨道工程任务的分析和设计；培养学生创新思维能力，为以后科学研究打下基础；了解目前轨道动力学中的热点问题和分析方法。

招生信息
硕士招生:
轨道设计与控制方向，包括轨道设计与分析、轨道控制与仿真、任务规划等方向

博士招生:
轨道动力学与控制方向，包括轨道机动、轨迹优化、不确定性分析、最优控制等方向

热烈欢迎飞行器设计专业、控制专业、数学专业的学生前来咨询报考！

Personal Introduction
Gang Zhang received the Bachelor’s degree from School of mathematics at Jilin University in 2007, and Ph.D. degree of Aerospace Engineering at Harbin Institute of Technology in 2012, respectively. He was a visiting student at the Department of Aerospace Engineering, Texas A&M University. Now he is a Full Professor in Harbin Institute of Technology. His current research interests include orbit rendezvous, orbit transfer, relative motion, and tangent orbit.

Address: Research Center of Satellite Technology, School of Astronautics, Harbin Institute of Technology, 150001, Harbin

Emai: zhanggang@hit.edu.cn; zhanggang3110@163.com;





Education
2003.9-2007.6, Mathematics, Jilin University, Bachelor

2007.8-2012.7, Aerospace Engineering, Harbin Institute of Technology, Ph.D.

2009.10-2010.10, Aerospace Engineering, Texas A&M University, Visiting student

Publications
1.Mingying Huo, Gang Zhang*, Naiming Qi, Yufei Liu, Xin Shi. Initial Trajectory Design of Electric Solar Wind Sail Based on Finite Fourier Series Shape-Based Method. IEEE Transactions on Aerospace and Electronic Systems, 2019, (accepted, SCI, IF: 2.063)

2.Gang Zhang*, Daniele Mortari. Second-Order Integral-Form Gauss's Variational Equations Under Impulsive Control.AIAA Journal of Guidance, Control, and Dynamics, 2019, 42(2): 284-302 (SCI,IF: 2.024)

3.ChengqingXie*, Wenfu Xu, Gang Zhang, Yingchun Zhang. Patched Shaping Approach toLow-Thrust Multi-Revolution Transfer Design. Proceedings of the Institution of MechanicalEngineers, Part G, Journal of Aerospace Engineering, 2018, (accepted,SCI, IF: 1.038)

4.Gang Zhang*, DiZhou, Daniele Mortari, Maruthi Akella. Covariance Analysis of Lambert’Problem via Lagrange's Transfer-Time Formulation. Aerospace Science and Technology,2018, 77: 765-773 (SCI, IF: 2.228)

5.Gang Zhang*, Yunhai Geng. Minimizing the Effects of Impulsive Orbit Maneuver Uncertainty. ASCE Journal of Aerospace Engineering, 2018, 31(5), **: 1-11 (SCI,IF: 1.296)

6.Gang Zhang*, DongYe. Optimal Short-Range Rendezvous Using On-Off Constant Thrust. Aerospace Science and Technology, 2017, 69: 209-217 (SCI, IF: 2.228)

7.Chengqing Xie, Gang Zhang*, Yingchun Zhang. ShapingApproximation for Low-Thrust Trajectories with Large Out-of-Plane Motion. AIAA Journal of Guidance, Control, and Dynamics, 2016, 39(12): 2776-2785. (SCI,IF: 2.024)

8.Gang Zhang*, XibinCao, DanieleMortari. AnalyticalApproximate Solutions to Ground Track Adjustment for Responsive Space. IEEE Transactions on Aerospace and Electronic Systems,2016, 52(3): 1366-1383. ( SCI, IF: 2.063)

9.Gang Zhang*, Jing Sheng. ImpulsiveGround-Track Adjustment for Assigned Final Orbit. AIAA Journal of Spacecraft and Rockets, 2016, 53(4): 599-609. (SCI, IF: 1.116)

10. Gang Zhang*, Xibin Cao. Coplanar Ground-Track Adjustment Using Time Difference. Aerospace Science and Technology, 2016, 48: 21-27 (SCI, IF: 2.228)

11. Chengqing Xie, Gang Zhang*, Yingchun Zhang. SimpleShaping Approximation for Low-Thrust Trajectories Between Coplanar EllipticalOrbits. AIAA Journal of Guidance, Control, and Dynamics, 2015, 38(12): 2448-2455. (SCI, IF: 2.024)

12. Gang Zhang*, Xibin Cao, Di Zhou. Two-Impulse Cotangent Rendezvous Between Coplanar Ellipticand Hyperbolic Orbits. AIAA Journal of Guidance, Control, and Dynamics,2014, 37(3): 964-969. (SCI, IF: 2.024)

13. Gang Zhang*, Di Zhou, Zhaowei Sun, Xibin Cao. Optimal Two-Impulse Cotangent Rendezvous Between Coplanar Elliptical Orbits. AIAA Journal of Guidance, Control, and Dynamics, 2013, 36(3): 677-685. (SCI, IF: 2.024)

14. Gang Zhang*, Di Zhou. Tangent Orbit Technique in Three Dimensions. AIAA Journal of Guidance, Control, and Dynamics, 2012, 35(6): 1907-1911. (SCI, IF: 2.024)

15. Gang Zhang*, Di Zhou, Daniele Mortari, Troy A. Henderson. Analytical Study of Tangent Orbit and Conditions for Its Solution Existence. AIAA Journal of Guidance, Control, and Dynamics, 2012, 35(1): 186-194. (SCI, IF: 2.024)

16. Gang Zhang*, Di Zhou, Xiaoli Bai. Tangent Orbital Rendezvous with the Same Direction of Terminal Velocities. AIAA Journal of Guidance, Control, and Dynamics, 2012, 35(1): 335-340. (SCI, IF: 2.024)

17. Gang Zhang*, Daniele Mortari, Di Zhou. Constrained Multiple-Revolution Lambert's Problem. AIAA Journal of Guidance, Control, and Dynamics, 2010, 33(6):1779-1786. (SCI, IF: 2.024)

18. Gang Zhang*, Guangfu Ma, Dongbai Li. Two-Impulse Transfer Between Coplanar Elliptic Orbits Using Along-Track Thrust. Celestial Mechanics and Dynamical Astronomy, 2015, 121(3): 261-274 (SCI, IF: 2.121)

19. Gang Zhang*, Di Zhou, Zhaowei Sun, Xibin Cao. Optimal Periodic Relative Orbit andRectilinear Relative Orbits with Eccentric Reference Orbits. Celestial Mechanics and Dynamical Astronomy, 2013, 117(2): 137-148. (SCI, IF: 2.121)

20. Gang Zhang*, Di Zhou, Daniele Mortari. Optimal Two-Impulse Rendezvous Using Constrained Multiple-Revolution Lambert Solutions. Celestial Mechanics and Dynamical Astronomy, 2011, 110(4): 305-317. (SCI, IF: 2.121)

21. Gang Zhang*, Di Zhou. A Second-Order Solution to the Two-Point Boundary Value Problem for Rendezvous in Eccentric Orbits. Celestial Mechanics and Dynamical Astronomy, 2010, 107(3): 319-336. (SCI, IF: 2.121)

22. Gang Zhang*, Xibin Cao, Guangfu Ma. Reachable Domain of Spacecraft with a Single Tangent Impulse Considering Trajectory Safety. Acta Astronautica, 2013, 91: 228-236 (SCI, IF: 2.227)

23. Gang Zhang*, Di Zhou, Daniele Mortari. An Approximate Analytical Method for Short-Range Impulsive Orbit Rendezvous Using Relative Lambert Solutions. Acta Astronautica, 2012, 81: 318-324.(SCI, IF: 2.227)

24. Gang Zhang*, Dongzhe Wang, Xibin Cao, Guangfu Ma. Minimum-time Interception with a TangentImpulse. ASCE Journal of Aerospace Engineering, 2015, 28(2), **:1-8. (SCI, IF: 1.296)

25. Gang Zhang*, Xiangyu Zhang, Xibin Cao. Tangent-Impulse Transfer from Elliptic Orbit to anExcess Velocity Vector. Chinese Journal of Aeronautics, 2014, 27(3): 577-583 (SCI, IF: 1.614)

26. Gang Zhang*,Di Zhou. An Improved Two-Manoeuvre Method for Orbit Rendezvous with Constant Thrust. Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering, 2012,226: 1583-1592. (SCI, IF: 1.038)

27. Gang Zhang*,Dongzhe Wang, Xibin Cao, Zhaowei Sun. Tangent Orbital Rendezvous Using Linear Relative Motion with J2 Perturbations. Mathematical Problems in Engineering, 2013, Article ID 531672: 1-8. (SCI, IF: 1.145)

28. Xiangyu Zhang, Gang Zhang*, Xibin Cao. Optimal Elliptic Orbital Maneuver with Continuous Radial Thrust on the Chaser Using Generating Functions. ASCE Journal of Aerospace Engineering, 2016, 29(1),**: 1-8 (SCI, IF: 1.296)

29. Chengqing Xie, Gang Zhang*, Yingchun Zhang, Huayi Li. Optimal Two-Impulse Rendezvous with Terminal Tangent Burn Considering the Trajectory Constraints. Advances in Space Research, 2014, 54(4): 734-743. (SCI, IF: 1.529)

30. Dongzhe Wang, Gang Zhang*, Xibin Cao. Tangent-Impulse Interception for a Hyperbolic Target. Mathematical Problems in Engineering,2014, Article ID 837849: 1-10. (SCI, IF: 1.145)

31. Di Zhou, Gang Zhang*. A Solution to Two-Point Boundary Value Problem for Power-Limited Rendezvous with Constant Thrust. Acta Astronautica, 2011,69(3-4): 150-157. (SCI, IF: 2.227)

32. Dongzhe Wang, Gang Zhang*, Xibin Cao. Modified Inverse-Polynomial Shaping Approach with Thrust and Radius Constraints. Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering, 2015, 229(13):2506-2518 (SCI, IF: 1.038)



(updateon March 9^th, 2019)











论文期刊

论文标题Shaping Approximation for Low-Thrust Trajectories with Large Out-of-Plane Motion

作者Chengqing Xie, Gang Zhang*, Yingchun Zhang

期刊名称AIAA Journal of Guidance, Control, and Dynamics

期卷39(12)



论文标题Analytical Approximate Solutions to Ground Track Adjustment for Responsive Space

作者Gang Zhang*, Xibin Cao, Daniele Mortari

期刊名称IEEE Transactions on Aerospace and Electronic Systems

期卷52(3)



论文标题Simple Shaping Approximation for Low-Thrust Trajectories Between Coplanar Elliptical Orbits

作者Chengqing Xie, Gang Zhang*, Yingchun Zhang

期刊名称AIAA Journal of Guidance, Control, and Dynamics

期卷38(12)



论文标题Two-Impulse Cotangent Rendezvous Between Coplanar Elliptic and Hyperbolic Orbits

作者Gang Zhang*, Xibin Cao, Di Zhou

期刊名称AIAA Journal of Guidance, Control, and Dynamics

期卷37(3)



论文标题Optimal Two-Impulse Cotangent Rendezvous Between Coplanar Elliptical Orbits

作者Gang Zhang*, Di Zhou, Zhaowei Sun, Xibin Cao

期刊名称AIAA Journal of Guidance, Control, and Dynamics

期卷36(3)



论文标题Tangent Orbit Technique in Three Dimensions

作者Gang Zhang*, Di Zhou

期刊名称AIAA Journal of Guidance, Control, and Dynamics

期卷35(6)



论文标题Analytical Study of Tangent Orbit and Conditions for Its Solution Existence

作者Gang Zhang*, Di Zhou, Daniele Mortari, Troy A. Henderson

期刊名称AIAA Journal of Guidance, Control, and Dynamics

期卷35(1)



论文标题Tangent Orbital Rendezvous with the Same Direction of Terminal Velocities

作者Gang Zhang*, Di Zhou, Xiaoli Bai

期刊名称AIAA Journal of Guidance, Control, and Dynamics

期卷35(1)



论文标题Constrained Multiple-Revolution Lambert@#%s Problem

作者Gang Zhang*, Daniele Mortari, Di Zhou

期刊名称AIAA Journal of Guidance, Control, and Dynamics

期卷33(6)



出版物
近年来一直从事飞行器轨道动力学与控制的研究工作，在轨道转移、轨道交会、相对运动和正切轨道等方向均有深入研究。以第一作者或通讯作者身份发表和录用学术论文近40篇，包括SCI收录30篇，EI收录4篇，其中有9篇发表在航空航天领域权威期刊AIAA Journal of Guidance, Control, and Dynamics上，1篇发表在航空航天顶级期刊 IEEE Transactions on Aerospace and Electronic Systems上。同时，长期担任Journal of Guidance, Control, and Dynamics, Celestial Mechanics and Dynamical Astronomy, Acta Astronautica,《航空学报》，《宇航学报》等航空航天国际国内重要期刊的审稿人。

重要期刊列表如下，详细列表见“English”板块