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Modal simulation and experimental verification of Space-borne two dimensional turntable

机译:星载二维转台的模态仿真与实验验证

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In order to avoid the resonance between the two dimensional turntable and the satellite, the modal simulation of the two dimensional turntable is carried out in this paper. And the simulation results are compared with the experimental results, combined with modal experiment, the simulation results before and after optimization are further verified. Firstly, two dimensional turntable as the research object in this paper, and it is modeled with the finite element method, then we use Patran/Nastran to conduct the modal simulation. In the modal simulation process, the bearing can be equivalent to the spring element, and the MPC element is used to instead of the spring element. And we introduce the modeling method of the MPC unit, the fundamental frequency of two dimensional turntable is obtained through modal simulation. At last, the model experiment is verified by hammering method, the frequency response functions in each direction of x, y and z are measured. Simulations and experimental results show: after optimization, the fundamental frequency of the two dimensional turntable is 42 Hz, which is higher than that of the base frequency 25 Hz, illustrating that the optimized structural design of the two dimensional turntable meets the requirements; The natural frequency and the experimental errors of three - dimensional turntable in x, y, z are 5%, which shows that MPC can simulate the bearing accurately, and is suitable for the simulation of two dimensional turntable.
机译:为了避免二维转盘与卫星之间的共振,本文对二维转盘进行了模态仿真。并将仿真结果与实验结果进行比较,并与模态实验相结合,进一步验证了优化前后的仿真结果。本文首先以二维转台为研究对象,并采用有限元方法对其进行建模,然后使用Patran / Nastran进行模态仿真。在模态仿真过程中,轴承可以等效于弹簧元件,而MPC元件代替弹簧元件。并介绍了MPC单元的建模方法,通过模态仿真获得了二维转台的基频。最后,通过锤击法对模型实验进行了验证,测量了x,y和z各方向的频率响应函数。仿真和实验结果表明:优化后的二维转盘基频为42Hz,高于基本频率25Hz,说明二维转盘的优化结构设计符合要求。三维转台在x,y,z处的固有频率和实验误差均为5%,说明MPC可以精确地模拟轴承,适合二维二维转台的仿真。

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