个人简历

Education background\r
1999 PhD from Harbin Institute of Technology in Space System Engineering\r
\r
Concurrent Academic\r
AIAA Senior Member\r
the Committee Member of Shanghai Key Lab of Intelligent Control of Space Vehicles\r
Associated Editor of The Scientific Would Journal\r
Associated Editor of Journal of Deep Space Exploration

研究领域

Orbit theory in irregular gravitational field\r
\r
Interplanetary mission analysis and optimization""

近期论文

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\r
\r
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\r
\r
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\r
\r
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\r
\r
Baoyin, H, Mcinnes, C, Solar sail orbits at artificial Sun-Earth libration points, Journal of guidance, control, and dynamics, 28(6)1328-1331,2005\r
\r
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\r
\r
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\r
\r
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\r
\r
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\r
\r
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\r
\r
Jin, Jin; Baoyin, Hexi; Li, Junfeng; Attitude scheme for satellite with defective inertia characteristic, Aircraft Engineering and Aerospace Technology, 85(5)422-431, 2013\r
\r
Baoyin, Hexi; Li, Junfeng; A survey on orbital dynamics and navigation of asteroid missions Acta Mechanica Sinica, 1, 2013\r
\r
Yu, Y, Baoyin, H, Orbital dynamics in the vicinity of asteroid 216 Kleopatra, The Astronomical Journal, 143(3)62-70,2012\r
\r
Gong, S, Li, J, Baoyin, H, Lunar landing trajectory design based on invariant manifold , Applied mathematics and mechanics, 28()201-207, 2007\r
\r
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\r
\r
Liu, X; Baoyin, H; Ma, X; Five special types of orbits around Mars, Journal of guidance, control, and dynamics, 33(4)1294-1301, 2010\r
\r
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\r
\r
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\r
\r
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\r
\r
Gao, Y; Baoyin, H; Li, J; Comparison of two methods in satellite formation flying , APPLIED MATHEMATICS AND MECHANICS, 24(8)902-908, 2003\r
\r
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\r
\r
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\r
\r
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\r
\r
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\r
\r
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\r
\r
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\r
\r
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\r
\r
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\r
\r
Baoyin, H; Chen, Y; Li, J; Capturing near earth objects, Research in Astronomy and Astrophysics, 10(6)587-,2010\r
\r
Yu, Y; Baoyin, H; Generating families of 3D periodic orbits about asteroids, Monthly Notices of the Royal Astronomical Society, 427(1)872-881, 2012\r
\r
Gong, S; Li, J; Baoyin, H; Formation reconfiguration in restricted three body problem , Acta Mechanica Sinica, 23(3)321-328, 2007\r
\r
Liu, X; Baoyin, H; Ma, X; Extension of the critical inclination, Astrophysics and Space Science, 334(1)115-124, 2011\r
\r
Gong, S; Li, J; Baoyin, H; Formation around planetary displaced orbit, Applied Mathematics and Mechanics, 28()759-767, 2007\r
\r
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\r
\r
Yu, Y; Baoyin, H; Resonant orbits in the vicinity of asteroid 216 Kleopatra, Astrophysics and Space Science, 343(1)75-82, 2013\r
\r
Gong, S; Baoyin, H; Li, J; Coupled attitude–orbit dynamics and control for displaced solar orbits, Acta Astronautica, 65(5)730-737, 2009\r
\r
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\r
\r
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\r
\r
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\r
\r
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\r
\r
Yu, Y; Baoyin, H; Li, J; Dynamic modelling and analysis of space webs, Science China Physics, Mechanics and Astronomy, 54(4)783-791, 2011\r
\r
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\r
\r
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\r
\r
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\r
\r
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\r
\r
Gong, S; Baoyin, H; Li, J; Solar sail three-body transfer trajectory design, Journal of guidance, control, and dynamics, 33(3)873-886, 2010\r
\r
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\r
\r
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\r
\r
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\r
\r
Gong, S; Li, J; Baoyin, H; Transfer trajectories design for a variable lightness solarcraft, Journal of Spacecraft and Rockets, 46(4)836-844, 2009\r
\r
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\r
\r
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\r
\r
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\r
\r
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\r
\r
Li, Y; Baoyin, H; 1st ACT global trajectory optimization competition: Tsinghua University results, Acta Astronautica, 61(9)735-741, 2007\r
\r
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\r
\r
Gong, S; Li, J; Baoyin, H; Relative motion around artificial lagrange points, Japan Society of Aeronautical Space Sciences Transactions, 51, 220-226, 2009\r
\r
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\r
\r
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\r
\r
Jiang, Y; Baoyin, H; Orbits and manifolds near the equilibrium points around a rotating asteroid, Astrophysics and Space Science, 349(1)83-106, 2014\r
\r
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\r
\r
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\r
\r
Baoyin, H; Li, J; Coupled trajectory and attitude stability of displaced orbits, Acta Mechanica Sinica, 26(1)127-140, 2010\r
\r
Y, CHEN; BAOYIN, H; J, LI; 木星探测轨道分析与设计, 天文学报, 53, 2, 2012\r
\r
Chen, Y; Baoyin, H; Li, J; Jupiter Exploration Mission Analysis and Trajectory Design, Acta Astronomica Sinica, 53, 106-118, 2012\r
\r
Gong, S; Li, J; Baoyin, H; A new solar sail orbit, Science China Technological Sciences, 55(3)848-855, 2012\r
\r
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\r
\r
Zeng, Xiangyuan; Baoyin, Hexi; Li, Junfeng; A solar sail inverse periodic orbit, Journal of Tsinghua University Science and Technology, 52(1)118-121, 2012\r
\r
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\r
\r
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\r
\r
Li, Jingyang; Gong, Shengping; Baoyin, Hexi; Generation of Multisegment Lunar Free-Return Trajectories, Journal of Guidance, Control, and Dynamics, 36(3)765-775, 2013\r
\r
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\r
\r
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