韩宏伟 照片

韩宏伟

助理教授

所属大学: 北京理工大学

所属学院: 宇航学院

邮箱:
hanhongweibit@bit.edu.cn

个人主页:
https://sae.bit.edu.cn/szdw20/szml/fxqgcx20/zjjqtjgryapypx/77b43c3da37f4602b226e682d13170cf.htm

个人简介

教育经历 2014-09 至 2020-03,北京理工大学,航空宇航科学与技术,博士 2010-09 至 2014-06,北京理工大学,飞行器设计与工程,学士 工作经历 2022-04 至 今,北京理工大学,宇航学院,预聘助理教授(特别副研究员) 2020-05 至 2022-04,北京理工大学,控制科学与工程流动站,博士后 获奖情况 2021年国际大学生立方星挑战赛中国赛区“优秀指导教师奖” 社会兼职 Astrodynamics、Defence Technology等期刊审稿人

研究领域

空天跨域飞行动力学与控制 天地往返制导与控制 在轨服务任务规划与决策

近期论文

Han H, Qiao D, Chen H, et al. Rapid Planning for Aerocapture Trajectory via Convex Optimization[J]. Aerospace Science and Technology, 2019, 84: 763-775. Han H, Qiao D, Chen H. Optimization of Aeroassisted Rendezvous and Interception Trajectories between Non-Coplanar Elliptical Orbits[J]. Acta Astronautica, 2019, 163: 190-200. Han H, Qiao D. Optimization for the Aeroassisted Orbital Plane Change with the Synergetic Maneuver Using the hp-Adaptive Pseudospectral Method[J]. Journal of Aerospace Engineering, 2017, 30(6): 04017076. Han H, Ren J, Li X. Transfer between libration orbits through the outer branches of manifolds for Phobos exploration[J]. Acta Astronautica, 2021, 189: 321-336. Jiang T, Han H. Fast and stable composite learning via high‐order optimization[J]. International Journal of Robust and Nonlinear Control, 2020, 30(17): 7731-7749. Jia F, Han H, Li X, Qiao D. Efficient optimization method for variable-specific-impulse low-thrust trajectories with shutdown constraint [J]. Science China Technological Sciences, 2021, online. Yao Q, Han H, Qiao D. Nonsingular fixed-time tracking guidance for Mars aerocapture with neural compensation[J]. IEEE Transactions on Aerospace and Electronic Systems, 2021, Online. 韩宏伟, 乔栋等.火星稀薄大气进入过程伞舱组合体振荡阻尼方法研究[J]. 中国科学: 技术科学, 2020, 50(9): 1140- 1149. Han H, Qiao D, Chen H. Optimal Ballistic Coefficient Control for Mars Aerocapture[C]. IEEE Chinese Guidance, Navigation and Control Conference, Nanjing, China, 2016: 2175-2180. Han H, Qiao D, Chen H. Coplanar Aerocapture Reachable Domain[C]. 26th International Symposium on Space Flight Dynamics, Matsuyama Ehime, Japan, 2017. Han H, Qiao D, Chen H. Optimal Aeroassisted Orbital Rendezvous and Interception [C]. 4th IAA Conference on Dynamics and Control of Space Systems, Changsha, China, 2018. Teng R, Qiao D, Han H. Numerical Predictive Entry Guidance for Mars Low-Lifting Vehicles[C]. IEEE Chinese Guidance, Navigation and Control Conference, Nanjing, China, 2016.