| 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 | 107 | 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 | 95 | 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 | 82 | 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 | 67 | 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 | 47 | 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 | 40 | 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 | 29 | 2017 |
| 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 | 29 | 2015 |
| Capturing near-Earth asteroids into bounded Earth orbits using gravity assist C Bao, H Yang, B Barsbold, H Baoyin Astrophysics and Space Science 360, 1-11, 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 | 26 | 2020 |
| Two-impulse transfer orbits connecting equilibrium points of irregular-shaped asteroids H Yang, S Gong, H Baoyin Astrophysics and Space Science 357, 1-11, 2015 | 23 | 2015 |
| Review of trajectory design and optimization for Jovian system exploration H Yang, J Hu, X Bai, S Li Space: Science & Technology 3, 0036, 2023 | 22 | 2023 |
| 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 | 21 | 2022 |
| 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 | 20 | 2021 |
| 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 |
| 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, 1-13, 2017 | 18 | 2017 |
| A particle-linkage model for non-axisymmetric elongated asteroids HW Yang, S Li, C Xu Research in Astronomy and Astrophysics 18 (7), 2018 | 15 | 2018 |
| 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 |
| Real-time trajectory optimization for collision-free asteroid landing based on deep neural networks Y Zhao, H Yang, S Li Advances in Space Research 70 (1), 112-124, 2022 | 14 | 2022 |
Shuang LiNanjing University of Aeronautics and AstronauticsE-mail confirmado em nuaa.edu.cn