A rotationalstiffness model for single-notch circular flexure hinge is established based on finite element method.
基于有限元方法建立了单切口柔性铰链旋转刚度模型。
2
Then the plan is to give the spacecraft some rotationalstiffness about the Y axis so the elevation angle can be controlled easily.
接下来会有一个关于Y轴转动刚度的计划给航空器好让仰角就可以很容易被控制。
3
Compared with the test results, the calculation methods of the initial rotationalstiffness and the bearing capacity and the mathematic model were testified to be true.