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Compare Tabletop style platform with umbrella style platform of air bearings spacecraft simulator

机译:比较桌上型平台与空气轴承航天器模拟器的伞型平台

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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.
机译:比较了3DOF航空航天模拟器的“桌面”和“伞”式平台。根据动弹性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公式。计算得出,空气轴承模拟器平台变形引起的不平衡转矩作用于重力。通过分析板与模拟器旋转中心之间的距离变化对不平衡扭矩的影响,可以比较这两种样式。结果表明,台式样式的平台具有比伞形样式更低的平衡敏感度,对有效载荷的适应性等优点。平台。但是,由于桌面式平台的空气轴承的旋转中心位于平台的板上,因此限制了模拟器的最大偏转角。

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