| Rapid satellite-to-site visibility determination based on self-adaptive interpolation technique C Han, XJ Gao, XC Sun Science China Technological Sciences 60, 264-270, 2017 | 35 | 2017 |
| Autonomous orbit determination via Kalman filtering of gravity gradients X Sun, P Chen, C Macabiau, C Han IEEE Transactions on Aerospace and Electronic Systems 52 (5), 2436-2451, 2016 | 32 | 2016 |
| Onboard satellite visibility prediction using metamodeling based framework X Wang, C Han, P Yang, X Sun Aerospace Science and Technology 94, 105377, 2019 | 26 | 2019 |
| Low-Earth orbit determination from gravity gradient measurements X Sun, P Chen, C Macabiau, C Han Acta Astronautica 123, 350-362, 2016 | 24 | 2016 |
| 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 | 19 | 2021 |
| Precise real-time navigation of LEO satellites using a single-frequency GPS receiver and ultra-rapid ephemerides X Sun, C Han, P Chen Aerospace Science and Technology 67, 228-236, 2017 | 17 | 2017 |
| 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 | 15 | 2020 |
| Real-time kinematic positioning of LEO satellites using a single-frequency GPS receiver P Chen, J Zhang, X Sun GPS Solutions 21, 973-984, 2017 | 15 | 2017 |
| Gravity gradient tensor eigendecomposition for spacecraft positioning P Chen, X Sun, C Han Journal of Guidance, Control, and Dynamics 38 (11), 2200-2206, 2015 | 15 | 2015 |
| APCHI technique for rapidly and accurately predicting multi-restriction satellite visibility X Sun, H Cui, C Han, G Tang Proc. Twenty-second AAS/AIAA Space Flight Mech. Meeting, 2012 | 15 | 2012 |
| Analytical field-of-regard representation for rapid and accurate prediction of agile satellite imaging opportunities H Wang, C Han, X Sun Journal of Astronomical Telescopes, Instruments, and Systems 5 (3), 037001 …, 2019 | 13 | 2019 |
| Optimization of low-thrust Earth-orbit transfers using the vectorial orbital elements Y Wang, C Han, X Sun Aerospace Science and Technology 112, 106614, 2021 | 12 | 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 | 12 | 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 | 12 | 2020 |
| New solution for rendezvous between geosynchronous satellites using low thrust S Zhang, C Han, X Sun Journal of Guidance, Control, and Dynamics 41 (6), 1397-1406, 2018 | 11 | 2018 |
| Instantaneous GNSS attitude determination: A Monte Carlo sampling approach X Sun, C Han, P Chen Acta Astronautica 133, 24-29, 2017 | 9 | 2017 |
| Algorithm of relative lambert transfer based on relative orbital elements H Chen, C Han, Y Rao, J Yin, X Sun Journal of Guidance, Control, and Dynamics 42 (6), 1413-1422, 2019 | 8 | 2019 |
| Autonomous orbit determination using epoch-differenced gravity gradients and starlight refraction C Pei, SUN Tengda, SUN Xiucong Chinese Journal of Aeronautics 30 (5), 1740-1749, 2017 | 8 | 2017 |
| Real-time precise orbit determination of LEO satellites using a single-frequency GPS receiver: Preliminary results of Chinese SJ-9A satellite X Sun, C Han, P Chen Advances in Space Research 60 (7), 1478-1487, 2017 | 8 | 2017 |
| High-precision attitude determination using spaceborne gravity gradiometer and gyroscope X Sun, X Mao, P Chen Acta Astronautica 200, 213-225, 2022 | 5 | 2022 |
