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DOF and Kinematic Analysis of a Deployable Truss Antenna Assembled by Tetrahedral Elements

机译:四面体单元组装的可展开桁架天线的自由度和运动学分析

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Deployable structure has played a more and more important role in the large-caliber antennas. This paper deals with the degree of freedom (DOF) and kinematics of a kind of deployable truss antenna composed of tetrahedral elements. Firstly, based on the reciprocal screw theory the DOF of one tetrahedral element is analyzed. Then, the equivalent mechanism of the minimum composite unit of the deployable truss antenna is obtained according to the characteristic of the DOF of the tetrahedral element. Sequentially, the DOF of the deployable truss antenna is derived. Further, the analytical expressions of the positions and velocities of the connection nodes of the antenna during its deploying/folding process are formulated by resorting to the coordinate transformation matrices. Finally, the correctness of the kinematic analysis of the deployable truss antenna is verified by simulation based on the Adams software.
机译:可展开结构在大口径天线中起着越来越重要的作用。本文研究了一种由四面体单元组成的可展开桁架天线的自由度(DOF)和运动学。首先,基于往复螺杆理论,分析了一个四面体单元的自由度。然后,根据四面体单元自由度的特性,获得了可展开桁架天线最小复合单元的等效机制。依次得出可展开桁架天线的自由度。此外,通过利用坐标变换矩阵来表达天线在其展开/折叠过程中的连接节点的位置和速度的解析表达式。最后,通过基于Adams软件的仿真,验证了可展开桁架天线运动学分析的正确性。

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