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个人信息Personal Information
教授 博士生导师
招生学科专业：
控制科学与工程 -- 【招收硕士研究生】 -- 航天学院
航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 航天学院
电子信息 -- 【招收硕士研究生】 -- 航天学院
机械 -- 【招收博士、硕士研究生】 -- 航天学院
性别：男
毕业院校：清华大学
学历：博士研究生毕业
学位：工学博士学位
所在单位：航天学院
办公地点：将军路校区D11楼B313
联系方式：邮箱：hongwei.yang@nuaa.edu.cn;
电子邮箱：
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- [1]杨洪伟,杨洪伟,杨彬,李爽,尤伟.基于不同动力引力辅助模型的木星转移轨道设计:上海航天,2019
- [2]杨洪伟,杨洪伟,李爽,杨洪伟,李爽,Bai, Xiaoli.Fast homotopy method for asteroid landing trajectory optimization using approximate initial costa...:J Guid Control Dyn,2019
- [3]杨洪伟,杨洪伟,宝音贺西.小行星附近制导与控制研究综述:深空探测学报,2019
- [4]杨洪伟,杨洪伟,李爽,Bai, Xiaoli.Fast Homotopy Method for Asteroid Landing Trajectory Optimization Using Approximate Initial Costa...
- [5]杨洪伟,李爽,李爽,杨洪伟,李爽,徐聪.A particle-linkage model for non-axisymmetric elongated asteroids:RESEARCH IN ASTRONOMY AND ASTROPHYSICS,2018
- [6]杨洪伟,杨洪伟,宝音贺西.小行星附近制导与控制研究综述
- [7]杨洪伟,杨洪伟,孙盼,李爽.太阳帆轨迹间接优化技术收敛性分析:中国科学:物理学 力学 天文学,2019
- [8]杨洪伟,杨洪伟,李爽,Bai, Xiaoli.Fast homotopy method for asteroid landing trajectory optimization using approximate initial costa...
- [9]Hongwei Yang,Shuang Li,Xiaoli Bai.Fast Homotopy Method for Asteroid Landing Trajectory Optimization Using Approximate Initial Costa....[J]:Journal of Guidance Control and Dynamics,2019,42(3):585-597
- [10]Hongwei Yang,,Xiaoli Bai,Hexi Baoyin.Rapid Trajectory Planning for Asteroid Landing with Thrust Magnitude Constraint.[J]:Journal of Guidance, Control, and Dynamics,2017,40(10):2713-2720
- [11]Hongwei Yang,杨洪伟,李爽,李爽,杨洪伟,Shuang Li,Xiaoli Bai,Bai, Xiaoli,李爽.Artificial Equilibrium Points near Irregular-Shaped Asteroids with Continuous Thrust.[J]:JOURNAL OF GUIDANCE CONTROL AND DYNAMICS,2018
- [12]Hongwei Yang,,Xiaoli Bai,Hexi Baoyin.Rapid Generation of Time-Optimal Trajectories for Asteroid Landing via Convex Optimization.[J]:Journal of Guidance Control and Dynamics,2017,40(3):628-641
- [13]Hongwei Yang,Xiaoli Bai,Hexi Baoyin.Finite-time control for asteroid hovering and landing via terminal sliding-mode guidance.[J]:Acta Astronautica,2017,132(78-89)
- [14]Hongwei Yang,Hexi Baoyin,Jingyang Li.Low-Cost Transfer between Asteroids with Distant Orbits Using Multiple Gravity Assists.[J]:Advances in Space Research,2015,56(5)
- [15]Hongwei Yang,Hexi Baoyin.Fuel-optimal control for soft landing on an irregular asteroid.[J]:IEEE Transactions on Aerospace and Electronic Systems,2015,51(3)
- [16]Hong-wei Yang,Hexi Baoyin,Xiang-yuan Zeng.Feasible Region and Stability Analysis for Hovering around Elongated Asteroids with Low Thrust.[J]:Research in Astronomy and Astrophysics,2015,15(9):1571-1586
- [17]Hongwei Yang,Hexi Baoyin,Shengping Gong.Two-impulse transfer orbits connecting equilibrium points of irregular-shaped asteroids.[J]:Astrophysics and Space Science,2015,357(1):66
- [18]Hongwei Yang,Hexi Baoyin,Yu Jiang.Fuel efficient control strategy for constellation orbital deployment.[J]:Aircraft Engineering and Aerospace Technology,2016,88(1):159-167
- [19]Changchun Bao,Hexi Baoyin,Hongwei Yang,Baza Barsbold.Capturing near-Earth asteroids into bounded Earth orbits using gravity assist.[J]:Astrophysics and Space Science,2015,360(2):61
- [20]Zhemin Chi,Hongwei Yang,Shiyu Chen,Junfeng Li.Homotopy Method for Optimization of Variable-Specific-Impulse Low-Thrust Trajectories.[J]:Astrophysics and Space Science,2017,362