对空气轴承航天器模拟器的桌面式平台与伞式平台进行了比较

Yanbin Li, Youhua Gao
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引用次数: 0

摘要

对空气轴承三维空间模拟器的“桌面”式平台和“伞”式平台进行了比较。根据运动弹性动力学分析理论和航天器姿态动力学理论,推导了平台结构质心位移的计算公式。计算了空气轴承模拟器平台在重力作用下的变形所产生的不平衡力矩。通过分析板与模拟器旋转中心之间距离变化对不平衡力矩的影响,可以比较两种方式的不平衡力矩。结果表明,台式平台比伞式平台具有平衡灵敏度低、载荷适应性强等优点。然而,由于台式平台空气轴承的旋转中心位于平台的平板上,限制了模拟器的最大偏转角度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Compare Tabletop style platform with umbrella style platform of air bearings spacecraft simulator
The “Tabletop” and “umbrella” style platforms of 3DOF air-bearing spacecraft simulator were compared. According to the theory on kineto-elastodynamic analysis and on the spacecraft attitude kinetics, the formulary for the platform structure mass-center displacement is deduced. It is calculated that the unbalance torque resulted from deforming of the platform of air-bearing simulator acted on gravity. Both of the styles can be compared by analyzing unbalance torque influence by changing of distance between the plate and the center of rotation of the simulator.The result shows that tabletop style platform has such advantages as lower equilibrium sensitivity, higher adaptability for payload than umbrella style platform. However, because the rotation center of air bearing of tabletop style platform locates the plate of the platform, the maximal deflection angle of the simulator was restricted.
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