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2012.9-2017.7 Ç廪´óѧ--º½Ì캽¿ÕѧԺ--º½¿ÕÓ¿ÆѧÓë¼¼Êõϵ²©Ê¿£¨ÍÆÃâÖ±²©£¬µ¼Ê¦£º±¦ÒôºØÎ÷½ÌÊÚ£¬Ç廪ÓŲ©±ÏÒµÉú/ÓŲ©ÂÛÎÄ£©
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[1]Yang H#, Bai X, Baoyin H. Rapid generation of time-optimal trajectories for asteroid landing via convex optimization[J]. Journal of Guidance, Control, and Dynamics, 2017, 40(3): 628-641. (SCI£¬º½Ì춯Á¦Ñ§Óë¿ØÖÆ·½Ïò¶¥¿¯)
[2]Yang H#, Bai X, Baoyin H. Rapid trajectory planning for asteroid landing with thrust magnitude constraint[J]. Journal of Guidance, Control, and Dynamics, 2017, 40(10): 1-8. (SCI£¬º½Ì춯Á¦Ñ§Óë¿ØÖÆ·½Ïò¶¥¿¯)
[3]Yang H#, Bai X, Li S. Artificial Equilibrium Points Near Irregular-shaped Asteroids with Continuous Thrust[J]. Journal of Guidance, Control, and Dynamics, 2018. (In press, SCI£¬º½Ì춯Á¦Ñ§Óë¿ØÖÆ·½Ïò¶¥¿¯)
[4]Yang H#, Baoyin H. Fuel-optimal control for soft landing on an irregular asteroid[J]. IEEE Transactions on Aerospace and Electronic Systems, 2015, 51(3): 1688-1697. (SCI)
[5]Yang H#, Bai X, Baoyin H. Finite-time control for asteroid hovering and landing via terminal sliding-mode guidance[J]. Acta Astronautica, 2017, 132: 78-89. (SCI)
[6]Yang H W#, Zeng X Y, Baoyin H. Feasible region and stability analysis for hovering around elongated asteroids with low thrust[J]. Research in Astronomy and Astrophysics, 2015, 15(9): 1571. (SCI)
[7]Yang H#, Gong S, Baoyin H. Two-impulse transfer orbits connecting equilibrium points of irregular-shaped asteroids[J]. Astrophysics and Space Science, 2015, 357(1): 66. (SCI)
[8]Yang H#, Li J, Baoyin H. Low-cost transfer between asteroids with distant orbits using multiple gravity assists[J]. Advances in Space Research, 2015, 56(5): 837-847. (SCI)
[9]Yang H#, Jiang Y, Baoyin H. Fuel efficient control strategy for constellation orbital deployment[J]. Aircraft Engineering and Aerospace Technology: An International Journal, 2016, 88(1): 159-167. (SCI)
[10]Yang H#, Baoyin H, Bai X, et al. Bounded trajectories near collinear-like equilibrium points of elongated asteroids using linear control[J]. Astrophysics and Space Science, 2017, 362(2): 27. (SCI)
[11]Chi Z, Yang H*, Chen S, et al. Homotopy method for optimization of variable-specific-impulse low-thrust trajectories[J]. Astrophysics and Space Science, 2017, 362(11): 216. (SCI)
[12]Wang W*, Yang H*, Zhang W, et al. Capture orbits around asteroids by hitting zero-velocity curves[J]. Astrophysics and Space Science, 2017, 362(12): 229. (SCI)
[13]Yang H#, Tang G, Jiang F. Optimization of observing sequence based on nominal trajectories of symmetric observing configuration[J]. Astrodynamics, 2018, 2(1): 25-37.
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