| Advances in dynamics and control of tethered satellite systems H Wen, DP Jin, HY Hu Acta Mechanica Sinica 24 (3), 229-241, 2008 | 184 | 2008 |
| Constrained tension control of a tethered space-tug system with only length measurement H Wen, ZH Zhu, D Jin, H Hu Acta Astronautica 119, 110-117, 2016 | 104 | 2016 |
| Output consensus and collision avoidance of a team of flexible spacecraft for on-orbit autonomous assembly T Chen, H Wen, H Hu, D Jin Acta Astronautica 121, 271–281, 2016 | 93 | 2016 |
| Distributed adaptive attitude control for networked underactuated flexible spacecraft T Chen, J Shan, H Wen IEEE Transactions on Aerospace and Electronic Systems 55 (1), 215 - 225, 2019 | 79 | 2019 |
| Space tether deployment control with explicit tension constraint and saturation function H Wen, ZH Zhu, D Jin, H Hu Journal of Guidance, Control, and Dynamics 39 (4), 915-920, 2016 | 76 | 2016 |
| Autonomous assembly with collision avoidance of a fleet of flexible spacecraft based on disturbance observer T Chen, H Wen Acta Astronautica 147, 86-96, 2018 | 70 | 2018 |
| Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations H Wen, DP Jin, HY Hu Nonlinear Dynamics 51, 501-514, 2008 | 64 | 2008 |
| On-orbit assembly of a team of flexible spacecraft using potential field based method T Chen, H Wen, H Hu, D Jin Acta Astronautica 133, 221-232, 2017 | 63 | 2017 |
| Distributed attitude tracking for multiple flexible spacecraft described by partial differential equations T Chen, H Wen, Z Wei Acta Astronautica 159, 637-645, 2019 | 51 | 2019 |
| Equivalent dynamic model for hoop truss structure composed of planar repeating elements F Liu, D Jin, H Wen AIAA Journal 55 (3), 1058-1063, 2017 | 44 | 2017 |
| 绳索系统的建模, 动力学和控制 金栋平， 文浩， 胡海岩 力学进展 34 (3), 304-313, 2004 | 43 | 2004 |
| Design and analysis of a vibration isolation system with cam–roller–spring–rod mechanism Y Zhang, G Wei, H Wen, D Jin, H Hu Journal of Vibration and Control 28 (13-14), 1781-1791, 2022 | 42 | 2022 |
| Model predictive control with output feedback for a deorbiting electrodynamic tether system H Wen, ZH Zhu, D Jin, H Hu Journal of Guidance, Control, and Dynamics 39 (10), 2451-2456, 2016 | 42 | 2016 |
| Coordinated motion control of a dual-arm space robot for assembling modular parts S Yang, H Wen, Y Hu, D Jin Acta Astronautica 177, 627-638, 2020 | 40 | 2020 |
| Ground experiment on rendezvous and docking with a spinning target using multistage control strategy Z Wei, H Wen, H Hu, D Jin Aerospace Science and Technology 104, 105967, 2020 | 40 | 2020 |
| Analytical deployment control law for a flexible tethered satellite system BS Yu, DP Jin, H Wen Aerospace Science and Technology 66, 294-303, 2017 | 38 | 2017 |
| Three-dimensional deployment of electro-dynamic tether via tension and current control with constraints H Wen, D Jin, H Hu Acta Astronautica 129, 253-259, 2016 | 35 | 2016 |
| Deployment of flexible space tether system with satellite attitude stabilization C Luo, H Wen, D Jin Acta Astronautica 160, 240-250, 2019 | 33 | 2019 |
| Fuzzy-logic-based robust attitude control of networked spacecraft via event-triggered mechanism S Xu, Z Wei, Z Huang, H Wen, D Jin IEEE Transactions on Aerospace and Electronic Systems 57 (1), 206-226, 2021 | 32 | 2021 |
| Experimental investigation on automated assembly of space structure from cooperative modular components Y Lu, Z Huang, W Zhang, H Wen, D Jin Acta Astronautica 171, 378-387, 2020 | 32 | 2020 |
Ti ChenNanjing University of Aeronautics and AstronauticsVerified email at nuaa.edu.cn