宝音贺西，全名宝音贺（西）喜格，男，蒙古族，1972年5月生，内蒙古扎赉特旗胡尔勒镇查干牧仁嘎查人，工学博士，教授，国家杰出青年基金获得者，中共党员。现任内蒙古工业大学党委副书记、校长。
1999年获哈尔滨工业大学飞行器设计专业博士学位，后赴日本、英国工作。2005年起任清华大学航天航空学院教授，2014-2017年连续入选Elsevier中国高被引学者榜单。攻克载人航天远距离最优导引关键技术并应用于交会对接工程，参与小行星捕获研究。2022年4月任内蒙古工业大学党委委员、副校长，2023年2月任常务副校长，2025年5月任现职。2024年4月在《自然·天文学》发表《Asteroid Kamo‘oalewa’s Journey from the Lunar Giordano Bruno Crater to Earth 1:1 Resonance》研究论文，发现2016HO3小行星来自月球背面布鲁诺撞击坑。主持内蒙古自治区“双碳”科技创新重大示范工程项目《适应高海拔低温型陆上大型国产化风电机组研制》，担任内蒙古自治区高等学校新型智库内蒙古能源战略研究中心负责人。2025年11月在深圳高交会“一带一路”国际产学研用合作会议作《从草原到云端：内蒙古低空经济发展的基础优势、实践探索与未来产业图景》主旨报告。曾获国家技术发明二等奖1项、军队科技进步一等奖、上海市科技进步一等奖，担任AIAA终身高级会员、Astrodynamics主编及《深空探测学报》《飞控与探测》编委。
中文名 | 宝音贺西 | 学位/学历 | 博士 |
|---|---|---|---|
本 名 | 宝音贺（西）喜格 | 职 业 | 教师 |
性 别 | 男 | 任职院校 | 内蒙古工业大学 |
国 籍 | 中国 | 职 称 | 教授 |
出生日期 | 1972年 | 政治面貌 | 中共党员 |
出生地 | 内蒙古扎赉特旗胡尔勒镇查干牧仁嘎查 | ||
毕业院校 | 哈尔滨工业大学 | 微信公众号/视频号 | |
专业方向 | 航天系统工程，行星际任务分析 | ||
人物经历
1999年，宝音贺西从哈尔滨工业大学飞行器设计专业获得博士学位；后在日本、英国等地工作。
2005年，来到清华大学工作。曾任清华大学航天航空学院航空宇航工程系教授。
2014-2017连续四年进入Elsevier公布的中国高被引学者航天工程方向榜单；曾获军队科技进步一等奖、上海市科技进步一等奖等；其小行星捕获、空间碎片发动机等成果两度被MIT Tech Review评论，引起广泛的国际关注。攻克载人航天远距离最优导引关键技术，研究成果应用与我国交会对接工程。
2022年4月，任内蒙古工业大学党委委员、副校长。
2023年2月，任内蒙古工业大学常务副校长。
2025年5月，任内蒙古工业大学党委副书记、校长。
中国人民政治协商会议内蒙古自治区第十三届委员会委员
职务任免
2025年5月，拟提名为自治区本科院校正职聘任人选。
学术兼职
AIAA终身高级会员、Astrodynamics主编, Science China，《深空探测学报》、《飞控与探测》编委等。
研究方向
Areas of Research Interests/ Research Projects
Space System Engineering, Interplanetary Mission Analysis, Satellite Control, Nonlinear Dynamics
Research Status
Orbit theory in irregular gravitational field
Interplanetary mission analysis and optimization
开展深空探测动力学与控制，相关基础理论及其在重大航天工程中的应用研究。
科研活动
宝音贺西参与过中国载人航天工程中的最优远距离导引策略设计工作，也参与过深空探测任务规划、新型卫星的任务优化等工作，并承担自然科学基金、863、973等科研项目。除了这些严肃的工作，他还做了一些颇为有趣的研究——小行星捕捉。
2024年4月19日，宝音教授团队在《自然·天文学》（Nature Astronomy）发表题目为《Asteroid Kamo‘oalewa’s Journey from the Lunar Giordano Bruno Crater to Earth 1:1 Resonance》的研究论文，发现我国“天问二号”任务的目标小行星 2016HO3 来自位于月球背面的布鲁诺撞击坑。
Education background
1999 PhD from Harbin Institute of Technology in Space System Engineering
Concurrent Academic
AIAA Senior Member
the Committee Member of Shanghai Key Lab of Intelligent Control of Space Vehicles
Associated Editor of The Scientific Would Journal
Associated Editor of Journal of Deep Space Exploration.
学术成果
发表论文
1. Baoyin, H, Mcinnes, C, Solar sail halo orbits at the Sun–Earth artificial L 1 point, Celestial Mechanics and Dynamical Astronomy, 94(2) 155-171, 2006
2. Baoyin, H, Li J, Gao Y, Dynamical behaviors and relative trajectories of the spacecraft formation flying, Aerospace science and technology, 6(4)295-301, 2002
3. Baoyin, H, Mcinnes, C, Solar sail equilibria in the elliptical restricted three-body problem, Journal of guidance, control, and dynamics, 29(3) 538-543, 2006
4. Baoyin, H, Mcinnes, C, Trajectories to and from the Lagrange Points and the Primary Body Surfaces, Journal of guidance, control, and dynamics, 29(4) 998-1003, 2006
5. Baoyin, H, Mcinnes, C, Solar sail orbits at artificial Sun-Earth libration points, Journal of guidance, control, and dynamics, 28(6)1328-1331,2005
6. Gong, S, Li, J, Baoyin, H, Passive Stability Design for Solar Sail on Displaced Orbits, Journal of Spacecraft and Rockets, 44(5)1071-1080, 2007
7. Jiang, F, Baoyin, H, Li, J, Practical techniques for low-thrust trajectory optimization with homotopic approach, Journal of Guidance, Control, and Dynamics, 35(1)245-258, 2012
8. Zhu, K, Li, J, Baoyin, H, Satellite scheduling considering maximum observation coverage time and minimum orbital transfer fuel cost, Acta Astronautica, 66(1) 220-229, 2010
9. Baoyin, Hexi; Yu, Yang; Li, Junfeng; Orbital Maneuver for a Rotating Tethered System via Tidal Forces, Journal of Spacecraft and Rockets, 50(5)1060-1068, 2013
10. Chen, Yang; Baoyin, Hexi; Li, Junfeng; Accessibility of Main-Belt Asteroids via Gravity Assists, Journal of Guidance, Control, and Dynamics, 37(2)623-632, 2014
11. Jin, Jin; Baoyin, Hexi; Li, Junfeng; Attitude scheme for satellite with defective inertia characteristic, Aircraft Engineering and Aerospace Technology, 85(5)422-431, 2013
12. Baoyin, Hexi; Li, Junfeng; A survey on orbital dynamics and navigation of asteroid missions Acta Mechanica Sinica, 1, 2013
13. Yu, Y, Baoyin, H, Orbital dynamics in the vicinity of asteroid 216 Kleopatra, The Astronomical Journal, 143(3)62-70,2012
14. Gong, S, Li, J, Baoyin, H, Lunar landing trajectory design based on invariant manifold , Applied mathematics and mechanics, 28201-207, 2007
15. Jiang, F; Li, J; Baoyin, H; Study on relative orbit geometry of spacecraft formations in elliptical reference orbits, Journal of guidance, control, and dynamics, 31(1)123-134, 2008
16. Liu, X; Baoyin, H; Ma, X; Five special types of orbits around Mars, Journal of guidance, control, and dynamics, 33(4)1294-1301, 2010
17. Gong, S; Li, J; Baoyin, H; Formation flying solar-sail gravity tractors in displaced orbit for towing near-earth asteroids, Celestial Mechanics and Dynamical Astronomy, 105(1)159-177, 2009
18. Zhou, X; Li, J; Baoyin, H; Equilibrium control of electrodynamic tethered satellite systems in inclined orbits, Journal of guidance, control, and dynamics, 29(6)1451-1454, 2006
19. Xue, D; Li, J; Baoyin, H; Jiang, F; Reachable domain for spacecraft with a single impulse, Journal of guidance, control, and dynamics, 33(3) 934-942, 2010
20. Gao, Y; Baoyin, H; Li, J; Comparison of two methods in satellite formation flying , APPLIED MATHEMATICS AND MECHANICS, 24(8)902-908, 2003
21. Jiang, F; Li, J; Baoyin, H; Approximate analysis for relative motion of satellite formation flying in elliptical orbits, Celestial Mechanics and Dynamical Astronomy, 98(1)31-66, 2007
22. Yuan, C; Li, J; Wang, T; Baoyin, Hi; Robust attitude control for rapid multi-target tracking in spacecraft formation flying, Applied mathematics and mechanics, 29185-198, 2008
23. Gong, S; Baoyin, H; Li, J; Solar sail formation flying around displaced solar orbits, Journal of guidance, control, and dynamics, 30(4)1148-1152, 2007
24. Liu, X; Baoyin, H; Ma, X; Equilibria, periodic orbits around equilibria, and heteroclinic connections in the gravity field of a rotating homogeneous cube, Astrophysics and Space Science, 333(2)409-418, 2011
25. Jiang, F; Li, J; Baoyin, H; Two-point boundary value problem solutions to spacecraft formation flying, Journal of guidance, control, and dynamics, 32(6)1827-1837, 2009
26. Liu, X; Baoyin, H; Ma, X; Periodic orbits in the gravity field of a fixed homogeneous cube, Astrophysics and Space Science, 334(2)357-364, 2011
27. Zhu, K; Jiang, F; Li, J; Baoyin, H; Trajectory optimization of multi-asteroids exploration with low thrust, Japan Society of Aeronautical Space Sciences Transactions, 5247-54, 2009
28. Zeng, X; Baoyin, H; Li, J; New applications of the H-reversal trajectory using solar sails, Research in Astronomy and Astrophysics, 11 7, 863-,2011
29. Baoyin, H; Chen, Y; Li, J; Capturing near earth objects, Research in Astronomy and Astrophysics, 10(6)587-,2010
30. Yu, Y; Baoyin, H; Generating families of 3D periodic orbits about asteroids, Monthly Notices of the Royal Astronomical Society, 427(1)872-881, 2012
31. Gong, S; Li, J; Baoyin, H; Formation reconfiguration in restricted three body problem , Acta Mechanica Sinica, 23(3)321-328, 2007
32. Liu, X; Baoyin, H; Ma, X; Extension of the critical inclination, Astrophysics and Space Science, 334(1)115-124, 2011
33. Gong, S; Li, J; Baoyin, H; Formation around planetary displaced orbit, Applied Mathematics and Mechanics, 28 759-767, 2007
34. Gong, S; Li, J; Baoyin, H; Analysis of displaced solar sail orbits with passive control, Journal of guidance, control, and dynamics, 31(3)782-785, 2008
35. Yu, Y; Baoyin, H; Resonant orbits in the vicinity of asteroid 216 Kleopatra, Astrophysics and Space Science, 343(1)75-82, 2013
36. Gong, S; Baoyin, H; Li, J; Coupled attitude–orbit dynamics and control for displaced solar orbits, Acta Astronautica, 65(5)730-737, 2009
37. Guo, T; Jiang, F; Baoyin, H; Fuel optimal low thrust rendezvous with outer planets via gravity assist, Science China Physics, Mechanics and Astronomy, 54(4)756-769, 2011
38. Chen, Y; Baoyin, H; Li, J; Trajectory design for the Moon departure libration point mission in full ephemeris model, Science China Technological Sciences, 54(11)2924-2934, 2011
39. Zhu, K; Li, J; Baoyin, H; Multi-swingby optimization of mission to Saturn using global optimization algorithms, Acta Mechanica Sinica, 25(6)839-845, 2009
40. Wang, J; Baoyin, H; Li, J; Optimal four-impulse rendezvous between coplanar elliptical orbits, Science China Physics, Mechanics and Astronomy, 54(4)792-802, 2011
41. Yu, Y; Baoyin, H; Li, J; Dynamic modelling and analysis of space webs, Science China Physics, Mechanics and Astronomy, 54(4)783-791, 2011
42. Liu, X; Baoyin, H; Ma, X; Analytical investigations of quasi-circular frozen orbits in the Martian gravity field, Celestial Mechanics and Dynamical Astronomy, 109(3)303-320, 2011
43. Liu, X; Baoyin, H; Ma, X; Long-term perturbations due to a disturbing body in elliptic inclined orbit , Astrophysics and Space Science, 339(2)295-304, 2012
44. Chen, Y; Baoyin, H; Li, J; Design and optimization of a trajectory for Moon departure Near Earth Asteroid exploration, Science China Physics, Mechanics and Astronomy, 54(4)748-755, 2011
45. Gong, S; Baoyin, H; Li, J; Multi-satellite reconfiguration of formation around libration point, Japan Society of Aeronautical Space Sciences Transactions, 51, 213-219, 2009
46. Gong, S; Baoyin, H; Li, J; Solar sail three-body transfer trajectory design, Journal of guidance, control, and dynamics, 33(3)873-886, 2010
47. Liu, X; Baoyin, H; Ma, X; Optimal path planning of redundant free-floating revolute-jointed space manipulators with seven links, Multibody System Dynamics, 29(1)41-56, 2013
48. Gong, S; Li, J; Baoyin, H; Solar radiation pressure used for formation flying control around the Sun-Earth libration point, Applied Mathematics and Mechanics, 30 1009-1016, 2009
49. Liu, X; Baoyin, H; Ma, X; Periodic orbits around areostationary points in the Martian gravity field, Research in Astronomy and Astrophysics, 12(5)551-,2012
50. Gong, S; Li, J; Baoyin, H; Transfer trajectories design for a variable lightness solarcraft, Journal of Spacecraft and Rockets, 46(4)836-844, 2009
51. Zeng, X; Baoyin, H; Li, J; Feasibility analysis of the angular momentum reversal trajectory via hodograph method for high performance solar sails, Science China Technological Sciences, 54(11)2951-2957, 2011
52. Gong, S; Baoyin, H; Li, J; Relative orbit design and control of formation around displaced solar orbits, Aerospace Science and Technology, 12(2)195-201, 2008
53. Zeng, X; Baoyin, H; Li, J; Three-dimensional time optimal double angular momentum reversal trajectory using solar sails, Celestial Mechanics and Dynamical Astronomy, 111(4)415-430, 2011
54. Gong, S; Li, J; Baoyin, H; Solar sail transfer trajectory from L1 point to sub-L1 point, Aerospace Science and Technology, 15(7)544-554, 2011
55. Li, Y; Baoyin, H; 1st ACT global trajectory optimization competition: Tsinghua University results, Acta Astronautica, 61(9)735-741, 2007
56. Baoyin, H; Liu, X; Beauvalet, L; Analysis of potential locations of asteroidal moonlets, Monthly Notices of the Royal Astronomical Society, 430(4)3483-3488, 2013
57. Gong, S; Li, J; Baoyin, H; Relative motion around artificial lagrange points, Japan Society of Aeronautical Space Sciences Transactions, 51, 220-226, 2009
58. Liu, X; Baoyin, H; Georgakarakos, N; The Hill stability of triple minor planets in the Solar system, Monthly Notices of the Royal Astronomical Society, 427(2)1034-1042, 2012
59. Zhang, P; Li, J; Baoyin, H; A low-thrust transfer between the Earth–Moon and Sun–Earth systems based on invariant manifolds, Acta Astronautica, 91, 77-88, 2013
60. Jiang, Y; Baoyin, H; Orbits and manifolds near the equilibrium points around a rotating asteroid, Astrophysics and Space Science, 349(1)83-106, 2014
61. J, QIN; BAOYIN, H; J, LI; 飞向 Halo 轨道的太阳帆航天器轨迹优化设计 , 清华大学学报 自然科学版, 47, 8, 2007
62. Liu, X; Baoyin, H; Ma, X; Motion planning for redundant prismatic-jointed manipulators in the free-floating mode, Acta Mechanica Sinica, 28(5)1449-1456, 2012
63. Baoyin, H; Li, J; Coupled trajectory and attitude stability of displaced orbits, Acta Mechanica Sinica, 26(1)127-140, 2010
64. Y, CHEN; BAOYIN, H; J, LI; 木星探测轨道分析与设计, 天文学报, 53, 2, 2012
65. Chen, Y; Baoyin, H; Li, J; Jupiter Exploration Mission Analysis and Trajectory Design, Acta Astronomica Sinica, 53, 106-118, 2012
66. Gong, S; Li, J; Baoyin, H; A new solar sail orbit, Science China Technological Sciences, 55(3)848-855, 2012
67. Liu, Xiaodong; Baoyin, Hexi; Marchis, Franck; The hierarchical stability of the seven known large size ratio triple asteroids using the empirical stability parameters, Astrophysics and Space Science, 1月4日 2013
68. Zeng, Xiangyuan; Baoyin, Hexi; Li, Junfeng; A solar sail inverse periodic orbit, Journal of Tsinghua University Science and Technology, 52(1)118-121, 2012
69. Guo, Tieding; Li, Junfeng; Baoyin, H; Pseudospectral Methods for Trajectory Optimization with Interior Point Constraints: Verification and Applications, Aerospace and Electronic Systems, IEEE Transactions on, 49(3)2005-2017, 2013
70. Liu, XiaoDong; Baoyin, HeXi; Ma, XingRui; Dynamics of surface motion on a rotating massive homogeneous body, Science China Physics, Mechanics and Astronomy, 56(4)818-829, 2013
71. Li, Jingyang; Gong, Shengping; Baoyin, Hexi; Generation of Multisegment Lunar Free-Return Trajectories, Journal of Guidance, Control, and Dynamics, 36(3)765-775, 2013
72. Wei, WANG; BAOYIN, Hexi; Junfeng, LI; 绳系卫星的动态释放变轨, 清华大学学报 (自然科学版, 48, 8, 2008)
73. H, YU; BAOYIN, He-xi; Jun-feng, LI; 双三体系统不变流形拼接成的低成本探月轨道, 宇航学报, 28, 3, 2007
工程应用
攻克载人航天远距离最优导引关键技术，研究成果应用与我国交会对接工程。
参与过深空探测任务规划、新型卫星的任务优化等工作，并承担自然科学基金、863、973等科研项目。
还做了一些关于“小行星捕捉”的研究。
获奖记录
军队科技进步一等奖
上海市科技进步一等奖等
人才培养
培养的博士生5人获得清华大学优秀博士论文奖，2人获得全国优秀博士论文奖。
家庭成员
有一姐：阿荣其其格，家中有七个兄弟姐妹。
相关链接
4、宝音贺西（内蒙古工业大学党委委员、常务副校长）-快懂百科
