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