H. Baoyin, Professor of Aerospace Engineering
Email:baoyin@tsinghua.edu.cn
Tel/Fax: +86-10-62795926
School of Aerospace, Tsinghua University, Mengminwei Science and Tech Building Room N903
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.
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
Academic Achievement
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, 28()201-207, 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, 29()185-198, 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, 52()47-54, 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
