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1. Wen H, Huang L, Xu S D, Jin D P. Angular velocity observer for space tether exploiting non-singular dynamics and vector measurements. Nonlinear Dynamics, 2021, 104(1): 399-410.
2. Luo C Q, Huang L, Wen H, Kang J J, Jin D P. Model predictive control for spin-up maneuver of an electrodynamic tether system. Acta Astronautica, 2021, 189: 55-62.
3. Pang Z J, Wen H, Rui X T, Du Z H. Nonlinear resonant analysis of space tethered satellite system in elliptical orbits. Acta Astronautica, 2021, 182: 264-273.
4. Luo C Q, Wen H, Jin D P, Xu S D. Dynamics of a flexible multi-tethered satellite formation in a Halo orbit with uncertain parameters. Communications in Nonlinear Science and Numerical Simulation, 2021, 99: 105828.
5. Xu S D, Wei Z T, Huang Z, Wen H, Jin D P. Fuzzy-logic-based robust attitude control of networked spacecraft via event-triggered mechanism. IEEE Transactions on Aerospace and Electronic Systems, 2021, 57(1): 206-226.
6. Huang L, Wen H, Cheng L, Xu S D. Nonlinear model predictive control for attitude maneuver of a barbell electric sail through voltage regulation. Acta Astronautica, 2021, 179: 146-152.
7. Cheng L, Wen H, Jin D P. Reconfiguration control of satellite formation using online quasi-linearization iteration and symplectic discretization. Aerospace Science and Technology, 2020, 107: 106348.
8. Luo C Q, Sun J L, Wen H, Jin D P. Dynamics of a tethered satellite formation for space exploration modeled via ANCF. Acta Astronautica, 2020, 177: 882-890.
9. Yang S J, Wen H, Hu Y H, Jin D P. Coordinated motion control of a dual-arm space robot for assembling modular parts. Acta Astronautica, 2020, 177, 627-638.
10. Xu S D, Wen H, Huang Z, Jin D P. A fuzzy control scheme for deployment of space tethered system with tension constraint, Aerospace Science and Technology, 2020, 106: 106143.
11. Ma J T, Wei Z T, Wen H, Jin D P. Boundary control of a Timoshenko beam with prescribed performance. Acta Mechanica, 2020, 231(8), 3219-3234.
12. Wei Z T, Wen H, Hu H Y, Jin D P. Ground experiment on rendezvous and docking with a spinning target using multistage control strategy, Aerospace Science and Technology, 2020, 104: 105967.
13. Xu S D, Wen H, Zheng H. Robust fuzzy sampled-data attitude control of spacecraft with actuator saturation and persistent disturbance. Aerospace Science and Technology, 2020, 101: 105850.
14. Lu Y, Huang Z, Zhang W, Wen H, Jin D P. Experimental investigation on automated assembly of space structure from cooperative modular components. Acta Astronautica, 2020, 171: 378-387.
15. Ma J T, Wen H, Jin D P. PDE model-based boundary control of a spacecraft with double flexible appendages under prescribed performance. Advances in Space Research, 2020: 65(1): 586-597.
16. Chen Y, Wen H, Jin D P. Design and experiment of a noncontact electromagnetic vibration isolator with controllable stiffness. Acta Astronautica, 2020, 168: 130-137.
17. 罗操群, 孙加亮, 文浩, 胡海岩, 金栋平. 多刚体系统分离策略及释放动力学研究. 力学学报, 52(2), 503-513, 2020.
18. 徐兴念, 文浩, 韦正涛. 基于超二次曲线障碍描述的航天器交会对接地面实验研究. 动力学与控制学报, 18(2), 42-49, 2020.
19. Wen H, Jin D P. De-spinning of tethered space target via partially invariable deployment with tension control. Nonlinear Dynamics, 2019, 96(1): 637-645.
20. Liu F S, Wang L B, Jin D P, Wen H. Equivalent continuum modeling of beam-like truss structures with flexible joints. Acta Mechanica Sinica, 2019, 35(5): 1067–1078.
21. Chen T, Shan J J, Wen H. Distributed passivity-based control for multiple flexible spacecraft with attitude-only measurements. Aerospace Science and Technology, 2019, 94: 105408.
22. Yang S J, Wen H, Jin D P. Trajectory planning of dual-arm space robots for target capturing and base manoeuvring. Acta Astronautica, 2019, 164: 142-151.
23. Cheng L, Wen H, Jin D P. Uncertain parameters analysis of powered-descent guidance based on Chebyshev interval method. Acta Astronautica, 2019, 162: 581-588.
24. Dang Q Q, Gui H C, Wen H. Dual-quaternion-based spacecraft pose tracking with a global exponential velocity observer. Journal of Guidance, Control, and Dynamics, 2019, 42(9): 2106-2115.
25. Dang Q Q, Gui H C, Xu M, Wen H. Dual-quaternion immersion and invariance velocity observer for controlling asteroid-hovering spacecraft. Acta Astronautica, 2019, 161: 304-312.
26. Luo C Q, Wen H, Jin D P. Deployment of flexible space tether system with satellite attitude stabilization. Acta Astronautica, 2019, 160: 240-250.
27. Chen T, Wen H, Wei Z T. Distributed attitude tracking for multiple flexible spacecraft described by partial differential equations. Acta Astronautica, 2019, 159: 637-645.
28. Chen T, Shan J, Wen H. Distributed adaptive attitude control for networked underactuated flexible spacecraft. IEEE Transactions on Aerospace and Electronic Systems, 2019, 55 (1): 215–225.
29. 张恒, 文浩, 罗操群. 旋转电动帆推进性能指标分析. 动力学与控制学报, 2019, 17(3): 281-287.
30. Wen H, Jin D P, Hu H Y. Removing singularity of orientation description for modeling and controlling an electrodynamic tether. Journal of Guidance, Control, and Dynamics, 2018, 41(3): 761-766.
31. Huang Z, Lu Y, Wen H, Jin D P. Ground-based experiment of capturing space debris based on artificial potential field. Acta Astronautica, 2018, 152: 235–241.
32. Luo C Q, Wen H, Jin D P. Libration control of bare electrodynamic tether for three-dimensional deployment. Astrodynamics, 2018, 2(3): 187–199.
33. Yu B S, Wen H, Jin D P. Review of deployment technology for tethered satellite systems. Acta Mechanica Sinica, 2018, 34(3): 754-768.
34. Chen T, Wen H. Autonomous assembly with collision avoidance of a fleet of flexible spacecraft based on disturbance observer. Acta Astronautica, 2018, 147: 86–96.
35. Ma J T, Jin D P, Wei Z T, Chen T Wen H. Boundary control of a flexible manipulator based on a high order disturbance observer with input saturation. Shock and Vibration, 2018: Article ID 2086424.
36. Wen H, Chen T, Jin D P, Hu H Y. Passivity-based control with collision avoidance for a hub-beam spacecraft. Advances in Space Research, 2017, 59(1): 425-433.
37. Wen H, Yu B S, Jin D P. Energy-based current control for stabilizing a flexible electrodynamic tether system. Journal of Beijing Institute of Technology, 2017, 26(1):1-4.
38. Yu B S, Jin D P, Wen H. An analytical control law of length rate for tethered satellite system. Meccanica. 2017, 52(9): 2035–2046.
39. Chen T, Wen H, Hu H Y, Jin D P. Distributed finite-time tracking for a team of planar flexible spacecraft. ISA Transactions, 2017, 69: 214–221.
40. Yu B S, Wen H. Vibroimpact dynamics of a tethered satellite system. Shock and Vibration, 2017: Article ID 8748094.
41. Yu B S, Jin D P, Wen H. Analytical deployment control law for a flexible tethered satellite system. Aerospace Science and Technology, 2017, 66: 294–303.
42. Liu F S, Jin D P, Wen H. Equivalent dynamic model for hoop truss structure composed of planar repeating elements. AIAA Journal, 2017, 55(3): 1058-1063.
43. Chen T, Wen H, Hu H Y, Jin D P. On-orbit assembly of a team of flexible spacecraft using potential field based method. Acta Astronautica, 2017, 133: 221–232.
44. Chen T, Wen H, Jin D P, Hu H Y. Quasi-time-optimal controller design for a rigid-flexible multibody system via absolute coordinate-based formulation. Nonlinear Dynamics, 2017, 88(1): 623–633.
45. Wu P C, Wen H, Chen T, Jin D P. Model predictive control of rigid spacecraft with two variable speed control moment gyroscopes. Applied Mathematics and Mechanics (English Edition), 2017, 38(11): 1551–1564.
46. 刘福寿, 金栋平, 文浩. 基于PDE模型的空间柔性曲梁无穷维Kalman滤波器设计. 中国科学: 物理学 力学 天文学, 2017, 47(10): 104611
47. 余瑶, 文浩, 陈提. 中心刚体-柔性梁应变反馈多目标优化控制. 动力学与控制学报, 2017, 15(4): 356-362.
48. Wen H, Jin D P, Hu H Y. Three-dimensional deployment of electro-dynamic tether via tension and current control with constraints. Acta Astronautica, 2016, 129: 253-259.
49. Wen H, Zhu Z H, Jin D P, Hu H Y. Model predictive control with output feedback for a deorbiting electrodynamic tether system. Journal of Guidance, Control, and Dynamics, 2016, 39(10): 2451-2456.
50. Wen H, Zhu Z H, Jin D P, Hu H Y. Exponentially convergent velocity observer for an electrodynamic tether in an elliptical orbit. Journal of Guidance, Control, and Dynamics, 2016, 39(5): 1112-1117.
51. Wen H, Zhu Z H, Jin D P, Hu H Y. Space tether deployment control with explicit tension constraint and saturation function. Journal of Guidance, Control, and Dynamics, 2016, 39(4): 915-920.
52. Wen H, Zhu Z H, Jin D P, Hu H Y. Tension control of space tether via online quasi-linearization iterations. Advances in Space Research, 2016, 57(3):754-763.
53. Wen H, Zhu Z H, Jin D P, Hu H Y. Constrained tension control of a tethered space-tug system with only length measurement. Acta Astronautica, 2016, 119:110-117.
54. Chu Y P, Wen H, Chen T. Nonlinear modeling and identification of an aluminum honeycomb panel with multiple bolts. Shock and Vibration, 2016: Article ID 1276753.
55. Liu F S, Jin D P, Wen H. Optimal vibration control of curved beams using distributed parameter models. Journal of Sound and Vibration, 2016, 384: 15-27.
56. Pang Z J, Jin D P, Yu B S, Wen H. Nonlinear normal modes of a tethered satellite system of two degrees of freedom under internal resonances. Nonlinear Dynamics, 2016, 85(3): 1779–1789.
57. Yu B S, Jin D P, Wen H. Nonlinear dynamics of a flexible tethered satellite system subject to space environment. Applied Mathematics and Mechanics, 2016, 37(4): 485-500.
58. Chen T, Wen H, Hu H Y, Jin D P. Output consensus and collision avoidance of a team of flexible spacecraft for on-orbit autonomous assembly. Acta Astronautica, 2016, 121: 271-281.
59. Chen T, Wen H, Jin D P, Hu H Y. New design and dynamic analysis for deploying rolled booms with thin wall. Journal of Spacecraft and Rockets. 2016, 53(1): 225-230.
60. 余本嵩, 文浩, 金栋平, 陈提. 空间电动力绳系统理论及实验研究. 力学进展, 2016, 46: 201605
61. Wu X J, Wen H, Chen T. Manoeuvres of spacecraft with flexible appendage in obstacle environment, International Journal of Space Science and Engineering, 2015, 3(1), 16-30.
62. 余本嵩, 文浩, 金栋平. 绳系卫星编队动力学及控制研究进展. 动力学与控制学报, 2015, 13(5): 321-328.
63. Jin D P, Wen H, Chen H. Nonlinear resonance of a subsatellite on a short constant tether. Nonlinear Dynamics, 2013, 71(3): 479-488.
64. 陈辉, 文浩, 金栋平, 胡海岩. 带刚性臂的空间绳系机构偏置控制. 中国科学: 物理学 力学 天文学, 2013, 43(4): 363-371.
65. 陈辉, 文浩, 金栋平, 胡海岩. 绳系卫星在轨试验及地面物理仿真进展. 力学进展, 2013, 43(1): 174-184.
66. 文浩, 陈辉, 金栋平, 胡海岩. 带可控臂绳系卫星释放及姿态控制. 力学学报, 44(2), 408-414, 2012.
67. 刘丽丽, 文浩, 金栋平, 胡海岩. 三维电动力绳系子卫星轨道转移的最优控制. 计算力学学报, 2011, 28(2): 178-182.
68. 文浩, 金栋平, 胡海岩. 绳系卫星收放控制地面实验研究. 振动工程学报, 2010, 23(1), 7-11.
69. 王晓宇, 文浩, 金栋平, 考虑姿态的绳系卫星后退时域回收控制. 力学学报, 2010, 42(5): 919-925.
70. Wen H, Jin D P, Hu H Y. Costate estimation for dynamic systems of the second order. Science in China Series E, 2009, 52(3): 752-760.
71. Wen H, Jin D P, Hu H Y. Feedback control for retrieving an electro-dynamic tethered sub-satellite. Tsinghua Science & Technology, 2009, 14(S2): 79-83.
72. 陈辉, 文浩, 金栋平, 胡海岩. 用弹性绳系系统进行空间捕捉的最优控制. 宇航学报, 2009, 30(2): 550-555.
73. 刘丽丽, 文浩, 金栋平, 胡海岩. 空间碎片对绳系卫星冲击的影响分析. 振动与冲击, 2009, 28(7): 12-16.
74. 刘丽丽, 文浩, 金栋平, 胡海岩. 绳系卫星轨道转移的最优控制研究. 航空学报, 2009, 30(2): 332-336.
75. Wen H, Jin D P, Hu H Y. Infinite-horizon control for retrieving a tethered subsatellite via an elastic tether. Journal of Guidance, Control, and Dynamics, 2008, 31(4): 899-906.
76. Wen H, Jin D P, Hu H Y. Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations. Nonlinear Dynamics, 2008, 51(4): 501-514.
77. Wen H, Jin D P, Hu H Y. Advances in dynamics and control of tethered satellite systems. Acta Mechanica Sinica, 2008, 24(3): 229-241.
78. Wen H, Jin D P, Hu H Y. Three-dimensional optimal deployment of a tethered subsatellite with an elastic tether. International Journal of Computer Mathematics, 2008, 85(6): 915-923.
79. 文浩, 金栋平, 胡海岩. 基于微分包含的绳系卫星时间最优释放控制. 力学学报, 2008, 40(1): 135-140.
80. 文浩, 金栋平, 胡海岩. 倾斜轨道电动力绳系卫星回收控制. 力学学报, 2008, 40(3): 375-380.
81. 刘丽丽, 文浩, 金栋平, 胡海岩. 三体绳系卫星面内编队飞行的回收控制. 振动工程学报, 2008, 21(3): 223-227.
82. 于明礼, 文浩, 胡海岩, 赵永辉. 二维翼段颤振的μ控制. 航空学报, 2007, 28(2), 340-343.
83. 于明礼, 文浩, 胡海岩. 二维翼段颤振的H∞控制. 振动工程学报, 2006, 19(3), 326-330.
84. 金栋平, 文浩, 胡海岩. 绳索系统的建模、动力学和控制.力学进展, 2004, 34 (3): 304-313.
[1] 文浩,文浩,文浩等.Nonlinear model predictive control for attitude maneuver of a barbell electric sail through voltage regulation.Acta Astronautica,2021
[2] 文浩,文浩,文浩等.Reconfiguration control of satellite formation using online quasi-linearization iteration and symplectic discretization.Aerospace Science and Technology,2020
[3] 文浩,胡海岩,胡海岩等.Ground experiment on rendezvous and docking with aspinning target using multistage control strategy.Aerospace Science and Technology,2020
[4] 文浩,文浩,文浩等.Coordinated motion control of a dual-arm space robot for assembling modular parts.Acta astronuatica,2020
[5] 文浩,文浩,文浩等.Boundary control of a Timoshenko beam with prescribed performance.Acta Mechanica,2020
[6] 文浩,文浩,文浩等.PDE model-based boundary control of a spacecraft with double flexible appendages under prescribed performance.Advances in Space Research,2020
[7] 文浩,文浩,文浩等.Experimental investigation on automated assembly of space structure from cooperative modular components.Acta Astronautica,2020
[8] 文浩,文浩,文浩等.Design and experiment of a noncontact electromagnetic vibration isolator with controllable stiffness.Acta Astronautica,2020
[9] 文浩,文浩,文浩等.多刚体系统分离策略及释放动力学研究.力学学报,2020
[10] 文浩,文浩,文浩等.基于超二次曲线障碍描述的航天器交会对接地面实验研究.动力学与控制学报,2020
[11] 文浩,陈提,陈提等.Distributed attitude tracking for multiple flexible spacecraft described by partial differential equations.Acta Astronautica,2019
[12] 文浩,罗操群,罗操群等.Deployment of flexible space tether system with satellite attitude stabilization.Acta Astronautica,2019
[13] 文浩,文浩,文浩等.Uncertain parameters analysis of powered-descent guidance based on Chebyshev interval method
[14] 文浩,杨书吉,杨书吉等.Trajectory planning of dual-arm space robots for target capturing and base manoeuvring.Acta Astronautica,2019
[15] 文浩,,等.De-spinning of tethered space target via partially invariable deployment with tension control.Nonlinear Dynamics,2019
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