Gravity balance technique installed on six-freedom spacecraft docking test table
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摘要: 为试验台主动对接环的重力平衡,研究了一种响应速度快、平衡力精度高,装在对接机构内部,适应高、低温环境的内装式重力平衡装置.介绍了有关技术:主动环实现三轴转动的球铰吊装机构;能够高速度、高精度地提供重力平衡力,并能实现自动随主动环上、下运动的智能型重力平衡技术;保证平衡器随主动环随动的轮轨式二维平动技术,经轻量化设计,其摩擦阻力和惯性阻力很小,并对轮/轨式方案进行了试验,当量摩擦系数仅为0.004 17.预计所研究装置的响应时间小于10 ms,各向失重模拟误差一般为1%~2%.Abstract: To balance gravity, a balance set with high respond speed and precision was designed. The set adaptable to high and low temperature was installed in the inside of the docking mechanism. Relative techniques are introduced, such as spherical gemel hoisting mechanism that made the active docking ring rotating in three-dimensional direction, intelligent gravity balance technique that could provide the force with high speed and precision to balance gravity and could automatically follow with the active docking ring, two-dimensional translation wheel technique that ensured balancer following the active docking ring. The friction and inertia resistance were very small by the design of lessening weight. An experiment about the wheel design was done. The results show that the equivalent weight friction coefficient is only 0.004 17. So the respond time of the whole design should be less that 10 ms. The error of simulated weightlessness is about 1%~2% in each direction.
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[1] 娄汉文,张柏楠,刘 宇. 空间对接机构试验技术[J]. 航天器工程,1994,3(3):23~30 Lou Hanwen, Zhang Bonan, Liu Yu. Test technology of space docking mechanism[J]. Spacecraft Engineering,1994,3(3):23~30(in Chinese) [2] 娄汉文,张柏楠. 空间对接机构的技术发展[J]. 航天工程,1994,3(3):1~22 Lou Hanwen, Zhang Bonan. The technical development of space docking mechanism[J]. Astronautical Engineering,1994,3(3):1~22(in Chinese) [3] Kiyomi Yolota. Test facility for rendezvous and docking system . 6th International Space Conference of Pacific Basin Societies , 1995,881~890 [4]Сироцятиков В С. Стнковочние устроцства космических аппаратов[M]. Машиностроение, 1984. 35~43 [5] 关英姿. 航天器对接过程的动力学及仿真技术研究 . 哈尔滨:哈尔滨工业大学航天工程系,2000 Guan Yingzi. Research on dynamics and simulation technique of spacecraft docking process . Harbin:Dept. of Astronautic Engineering and Mechanics, Harbin Institute of Technology, 2000(in Chinese) [6] 关英姿,崔乃刚,刘育华. 空间飞行器对接动力学的数值仿真研究[J]. 哈尔滨:哈尔滨工业大学学报,1999,31(4):121~124 Guan Yingzi,Cui Naigang,Liu Yuhua.Numerical simulation of spacecraft docking Dynamics[J]. Harbin:Journal of Harbin Institute of Technology,1999,31(4):121~124(in Chinese)
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