并对该气浮台的关键技术问题进行了探讨。
The key technical problem on air-floating platform was discussed.
最后，结合五自由度气浮台开发，深入研究了气浮台的转动惯量辨识算法。
Finally, combining the development of the air bearing simulator, algorithm of identifying the air bearing is researched.
结果表明由于平台变形使主惯性轴方向变化从而使气浮台姿态准确度产生误差。
The result shows that the deformation of platform makes the change on the direction of inertia principal axes which results in an error on the attitude precision.
本文利用三轴全物理仿真气浮台作为控制对象，模拟航天器在外层空间所受扰动力矩很小的力学环境。
Mechanical environment where spacecraft disturbance torque is very small in out space is simulated making use of a three-axis full physics air-bearing table as controlled object.
本文利用三轴全物理仿真气浮台作为控制对象，模拟航天器在外层空间所受扰动力矩很小的力学环境。
Mechanical environment where spacecraft disturbance torque is very small in out space is simulated making use of a three-axis full physics air-bearing table as controlled object.
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