| Sliding-mode impact time guidance law design for various target motions Q Hu, T Han, M Xin Journal of Guidance, Control, and Dynamics 42 (1), 136-148, 2019 | 120 | 2019 |
| New impact time and angle guidance strategy via virtual target approach Q Hu, T Han, M Xin Journal of Guidance, Control, and Dynamics 41 (8), 1755-1765, 2018 | 101 | 2018 |
| Three-dimensional guidance for various target motions with terminal angle constraints using twisting control Q Hu, T Han, M Xin IEEE Transactions on Industrial Electronics 67 (2), 1242-1253, 2019 | 60 | 2019 |
| Analytical solution of field-of-view limited guidance with constrained impact and capturability analysis T Han, Q Hu, M Xin Aerospace Science and Technology 97, 105586, 2020 | 37 | 2020 |
| Sensor-based robust incremental three-dimensional guidance law with terminal angle constraint T Han, Q Hu, HS Shin, A Tsourdos, M Xin Journal of Guidance, Control, and Dynamics 44 (11), 2016-2030, 2021 | 35 | 2021 |
| Analytical solution for nonlinear three-dimensional guidance with impact angle and field-of-view constraints Q Hu, T Han, M Xin IEEE Transactions on Industrial Electronics 68 (4), 3423-3433, 2020 | 32 | 2020 |
| Differentiator-based incremental three-dimensional terminal angle guidance with enhanced robustness T Han, HS Shin, Q Hu, A Tsourdos, M Xin IEEE Transactions on Aerospace and Electronic Systems 58 (5), 4020-4032, 2022 | 30 | 2022 |
| Incremental twisting fault tolerant control for hypersonic vehicles with partial model knowledge T Han, Q Hu, HS Shin, A Tsourdos, M Xin IEEE Transactions on Industrial Informatics 18 (2), 1050-1060, 2021 | 29 | 2021 |
| Three-dimensional approach angle guidance under varying velocity and field-of-view limit without using line-of-sight rate T Han, Q Hu, M Xin IEEE Transactions on Systems, Man, and Cybernetics: Systems 52 (11), 7148-7159, 2022 | 24 | 2022 |
| Field-of-view limited guidance with impact angle constraint and feasibility analysis Q Hu, R Cao, T Han, M Xin Aerospace Science and Technology 114, 106753, 2021 | 24 | 2021 |
| Robust autopilot design for STT missiles with multiple disturbances using twisting control T Han, Q Hu Aerospace Science and Technology 70, 428-434, 2017 | 17 | 2017 |
| Two-stage guidance law with constrained impact via circle involute Z Wang, Q Hu, T Han, M Xin IEEE Transactions on Aerospace and Electronic Systems 57 (2), 1301-1316, 2020 | 16 | 2020 |
| Barrier Lyapunov function based model predictive control of a morphing waverider with input saturation and full-state constraints P Dai, B Yan, T Han, S Liu IEEE Transactions on Aerospace and Electronic Systems 59 (3), 3071-3081, 2022 | 14 | 2022 |
| Three-dimensional impact time and angle guidance via controlling line-of-sight dynamics T Han, Y Xi, G Chen, Q Hu 2020 Chinese Control And Decision Conference (CCDC), 2850-2855, 2020 | 8 | 2020 |
| 大气层外动能拦截器末制导律与能量优化方法 郭建国， 韩拓， 周军， 王国庆 系统工程与电子技术 39 (2), 376-382, 2017 | 4 | 2017 |
| Constrained 3-D trajectory planning for aerial vehicles without range measurement T Han, Q Hu, Q Wang, M Xin, HS Shin IEEE Transactions on Systems, Man, and Cybernetics: Systems, 2024 | 3 | 2024 |
| Design of missile incremental adaptive fault tolerant control system Y FANG, Y LU, T HAN, Q HU 北京航空航天大学学报 48 (5), 920-928, 2022 | 3 | 2022 |
| Field-of-View Limited Guidance with Constrained Impact via Line-of-Sight Shaping Approach Y Xi, T Han, Q Hu, K Zhong 2019 Chinese Control And Decision Conference (CCDC), 2974-2978, 2019 | 3 | 2019 |
| 基于终端角度约束的二阶滑模制导律设计 郭建国， 韩拓， 周军， 王国庆 航空学报 38 (2), 210-219, 2017 | 3 | 2017 |
| 导引头量测故障下的增量式三维制导律设计 方艺忠， 韩拓， 胡庆雷 宇航学报 43 (4), 508-517, 2022 | 2 | 2022 |
