| Rapid Generation of Time-Optimal Trajectories for Asteroid Landing via Convex Optimization H Yang, X Bai, H Baoyin Journal of Guidance, Control, and Dynamics 40 (3), 628-641, 2017 | 97 | 2017 |
| Fuel-optimal control for soft landing on an irregular asteroid H Yang, H Baoyin IEEE Transactions on Aerospace and Electronic Systems 51 (3), 1688 - 1697, 2015 | 85 | 2015 |
| Fast Homotopy Method for Asteroid Landing Trajectory Optimization Using Approximate Initial Costates H Yang, S Li, X Bai Journal of Guidance, Control, and Dynamics 42 (3), 585-597, 2019 | 72 | 2019 |
| Finite-time control for asteroid hovering and landing via terminal sliding-mode guidance H Yang, X Bai, H Baoyin Acta Astronautica 132, 78-89, 2017 | 65 | 2017 |
| Low-cost transfer between asteroids with distant orbits using multiple gravity assists H Yang, J Li, H Baoyin Advances in Space Research 56 (5), 837-847, 2015 | 44 | 2015 |
| Homotopy Method for Optimization of Variable-Specific-Impulse Low-Thrust Trajectories Z Chi, H Yang, S Chen, J Li Astrophysics and Space Science 362 (11), 216, 2017 | 36 | 2017 |
| Optimization of observing sequence based on nominal trajectories of symmetric observing configuration H Yang, G Tang, F Jiang Astrodynamics 2 (1), 25–37, 2018 | 29 | 2018 |
| Rapid Trajectory Planning for Asteroid Landing with Thrust Magnitude Constraint H Yang, X Bai, H Baoyin Journal of Guidance, Control, and Dynamics 40 (10), 2713-2720, 2017 | 28 | 2017 |
| Capturing near-Earth asteroids into bounded Earth orbits using gravity assist C Bao, H Yang, B Barsbold, H Baoyin Astrophysics and Space Science 360 (2), 61, 2015 | 28 | 2015 |
| Feasible Region and Stability Analysis for Hovering around Elongated Asteroids with Low Thrust H Yang, XY Zeng, H Baoyin Research in Astronomy and Astrophysics 15 (9), 1571-1586, 2015 | 28 | 2015 |
| Fuel-optimal Asteroid Descent Trajectory Planning using a Lambert Solution-based Costate Initialization H Yang, S Li IEEE Transactions on Aerospace and Electronic Systems 56 (6), 4338-4352, 2020 | 23 | 2020 |
| Two-impulse transfer orbits connecting equilibrium points of irregular-shaped asteroids H Yang, S Gong, H Baoyin Astrophysics and Space Science 357 (1), 66, 2015 | 21 | 2015 |
| Artificial Equilibrium Points near Irregular-Shaped Asteroids with Continuous Thrust H Yang, X Bai, S Li Journal of Guidance, Control, and Dynamics 41 (6), 1308-1319, 2018 | 19 | 2018 |
| Fast computation of the Jovian-moon three-body flyby map based on artificial neural networks H Yang, J Yan, S Li Acta Astronautica 193, 710-720, 2022 | 18 | 2022 |
| Retrograde near-circular periodic orbits near equatorial planes of small irregular bodies L Lan, H Yang, H Baoyin, J Li Astrophysics and Space Science 362 (9), 169, 2017 | 18 | 2017 |
| Collision-free Trajectory Design for Long-distance Hopping Transfer on Asteroid Surface using Convex Optimization X Liu, H Yang, S Li IEEE Transactions on Aerospace and Electronic Systems 57 (5), 3071-3083, 2021 | 17 | 2021 |
| Artificial equilibrium points in binary asteroid systems with continuous low-thrust S Bu, S Li, H Yang Astrophysics and Space Science 362, 137, 2017 | 15 | 2017 |
| A particle-linkage model for non-axisymmetric elongated asteroids HW Yang, S Li, C Xu Research in Astronomy and Astrophysics 18 (7), 2018 | 14 | 2018 |
| Bounded trajectories near collinear-like equilibrium points of elongated asteroids using linear control H Yang, H Baoyin, X Bai, J Li Astrophysics and Space Science 362 (2), 27, 2017 | 12 | 2017 |
| Fuel efficient control strategy for constellation orbital deployment H Yang, Y Jiang, H Baoyin Aircraft Engineering and Aerospace Technology 88 (1), 159-167, 2016 | 12 | 2016 |
Shuang LiNanjing University of Aeronautics and Astronautics在 nuaa.edu.cn 的电子邮件经过验证
