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

机译:比较桌面风格平台与空气轴承伞式平板飞船模拟器

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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“桌面”和“伞形”轴承航天器模拟器的风格平台。根据KINETO-ELSTOTOM动力学分析和航天器姿态动力学的理论,推导了平台结构质量置换的公式。计算出不平衡扭矩因由引起的承气模拟器平台的变形而导致的不平衡扭矩。通过通过改变板与模拟器的旋转中心之间的距离来分析不平衡扭矩影响,可以通过分析不平衡扭矩影响来进行比较。结果表明,桌面风格平台具有较低的平衡敏感性,高度适应性高于伞式的优势平台。但是,由于桌面样式平台的空气轴承旋转中心定位了平台的板,所以模拟器的最大偏转角度受到限制。

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