| Design of agile satellite constellation based on hybrid-resampling particle swarm optimization method X Wang, H Zhang, S Bai, Y Yue Acta Astronautica 178, 595-605, 2021 | 48 | 2021 |
| Visibility optimization of satellite constellations using a hybrid method C Han, S Bai, S Zhang, X Wang, X Wang Acta Astronautica 163, 250-263, 2019 | 37 | 2019 |
| Novel method to calculate satellite visibility for an arbitrary sensor field C Han, Y Zhang, S Bai, X Sun, X Wang Aerospace Science and Technology 112, 106668, 2021 | 26 | 2021 |
| New fly-around formations for an elliptical reference orbit S Bai, C Han, Y Rao, X Sun, Y Sun Acta Astronautica 171, 335-351, 2020 | 19 | 2020 |
| Hovering formation control based on two-stage constant thrust C Han, S Bai, X Sun, Y Rao Journal of Guidance, Control, and Dynamics 43 (3), 504-517, 2020 | 15 | 2020 |
| Geometric analysis of ground-target coverage from a satellite by field-mapping method C Han, Y Zhang, S Bai Journal of Guidance, Control, and Dynamics 44 (8), 1469-1480, 2021 | 14 | 2021 |
| Teardrop hovering formation for elliptical orbit considering J2 perturbation S Bai, C Han, X Sun, H Zhang, Y Jiang Aerospace Science and Technology 106, 106098, 2020 | 14 | 2020 |
| A versatile method for target area coverage analysis with arbitrary satellite attitude maneuver paths H Wang, S Bai Acta Astronautica 194, 242-254, 2022 | 11 | 2022 |
| Geometric analysis of a constellation with a ground target Y Zhang, S Bai, C Han Acta Astronautica 191, 510-521, 2022 | 10 | 2022 |
| Coverage Analysis for Elliptical-Orbit Satellites Based on 2-D Map S Bai, Y Zhang, Y Jiang, Y Chen IEEE Transactions on Aerospace and Electronic Systems 59 (4), 4223-4239, 2023 | 9 | 2023 |
| Extended 2D Map for Satellite Coverage Analysis Considering Elevation-Angle Constraint Y Gu, Y Chen, Y Zhang, G Wu, S Bai IEEE Transactions on Aerospace and Electronic Systems, 2024 | 8 | 2024 |
| Finite-Thrust Lambert Transfer Based on Multistage Constant-Vector Thrust Control S Bai, Y Wang, H Liu, X Sun IEEE Transactions On Aerospace and Electronic Systems 59 (5), 4947-4967, 2023 | 8 | 2023 |
| Low-thrust Lambert transfer based on two-stage constant-vector thrust control method X Sun, S Bai Nonlinear Dynamics 110 (1), 313-346, 2022 | 8 | 2022 |
| Spacecraft fast fly-around formations design using the parallelogram configuration S Bai, Y Wang, H Liu, X Sun Nonlinear Dynamics 113 (2), 1041-1062, 2025 | 5 | 2025 |
| Minimum-observation method for rapid and accurate satellite coverage prediction S Bai, Y Zhang, Y Jiang GPS Solutions 26 (4), 110, 2022 | 5 | 2022 |
| Practical maintenance strategies for teardrop hovering formation relative to elliptical orbit S Bai, C Han, X Sun, Y Rao Acta Astronautica 190, 176-193, 2022 | 5 | 2022 |
| Exoatmospheric Intercept Guidance Based on Relative-Motion Control with Respect to Zero-Effort Orbit S Bai, H Chen, S Zhang, C Geng, C Han, M Xu Space: Science & Technology 4, 0112, 2024 | 4 | 2024 |
| Modified two-dimensional coverage analysis method considering various perturbations S Bai, Y Zhang, Y Jiang, W Sun, W Shao IEEE Transactions on Aerospace and Electronic Systems 60 (3), 2763-2777, 2023 | 4 | 2023 |
| Prediction Method of Agile Satellite's In-View Periods Based on Analytical Bounding Curves S Bai, Y Chen, Y Zhang IEEE Transactions on Aerospace and Electronic Systems, 2024 | 2 | 2024 |
| Geometric-Based Method for Regional-Target Coverage Analysis Y Zhang, C Han, W Sun, W Shao, S Bai IEEE Transactions on Aerospace and Electronic Systems 59 (3), 2252-2265, 2022 | 2 | 2022 |
