Reticular deployable antenna deploying process cable force analysis method

A technology of deployment process and analysis method, which is applied in the field of cable force analysis during the deployment process of mesh deployable antennas, and can solve problems such as deviation, error of analysis results, difficulty in meeting engineering requirements, etc.

Active Publication Date: 2015-04-29
XIDIAN UNIV
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Problems solved by technology

In this approximation method, the loading time of the cable net tension on the truss is generally set by engineers based on experience, which lacks theoretical basis; at the same time, it is assumed that the tension of the cable and the deployment time change linearly, which also deviates from the actual situation. Eventually lead to large errors in the analysis results
There are also researches on modeling and analysis methods based on a large number of cable-strut elements approximating curved cables. However, it is difficult to meet the engineering requirements in terms of calculation amount and approximation error.

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  • Reticular deployable antenna deploying process cable force analysis method
  • Reticular deployable antenna deploying process cable force analysis method
  • Reticular deployable antenna deploying process cable force analysis method

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Embodiment Construction

[0072] Such as image 3 As shown, the present invention provides a method for analyzing the cable force during the unfolding process of the deployable mesh antenna, comprising the following steps:

[0073] Step 101: See figure 1 , select the number N of truss units around the mesh expandable antenna (the number of connection points between the truss and the cable net is 2N), the length L of the truss unit cross bar 2 and vertical bar 1 1 and L 2 , the material parameter D of the cable net, the geometric parameter S, the topological structure of the cable net, and the number of working conditions M that determine the discreteness of the unfolding process;

[0074] Step 102: Calculate the position P of the connection point between the truss and the cable net around the deployable mesh antenna 0 j With the expansion angle θ={θ j} changing trajectory, where θ j ∈[0,90](j=1,2,...,M); such as Figure 4 As shown, this step includes the following steps:

[0075] Step 201: see ...

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Abstract

The invention provides a reticular deployable antenna deploying process cable force analysis method. The reticular deployable antenna deploying process cable force analysis method mainly includes steps: selecting the number and geometric parameters of peripheral truss units of a reticular deployable antenna, a material parameter D of a cable net, a geometric parameter S, a network cable topology structure and the number M of discrete working conditions of a deploying process; calculating a change motion trail of positions of connection points of trusses and the cable net; calculating a stress state of each cable unit under each working condition; fitting a changing curve F(theta) of acting force of the cable net for a boundary connection point along with changes of a spread angle; finally, using changing cable net acting force as a load, substituting the load into a flexible multiple body dynamics model, and performing dynamics analysis. The reticular deployable antenna deploying process cable force analysis method regards the deploying process of the reticular deployable antenna as a series of discrete loaded mechanism balance forms, studies strain distribution of each balance form, accurately obtains a cable force changing curve of the deploying process, and provides effective support for ground engineering to achieve influence mechanism analysis of cable net tension for the deploying process based on flexible multiple body system dynamics modeling and analysis.

Description

technical field [0001] The invention relates to the technical field of boundary motion cable structure tension analysis and its application, in particular to a cable force analysis method during the deployment process of a mesh-like deployable antenna. Background technique [0002] The deployment process of deployable antenna is a complex nonlinear mechanical process, which is the transformation from unstable state to stable state, and from mechanism to structure. The smooth deployment in orbit is the basis for the application of deployable antennas, and it is also one of the links most prone to failure. Therefore, in the design stage, the nonlinear influencing factors such as flexibility, friction, and cable net tension are accurately analyzed to realize the prediction of the dynamic behavior of the antenna deployment process, which has a guiding role in improving and perfecting the structural design of the antenna. The reflector cable net is gathered in the middle of the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F19/00
Inventor 张逸群茹文锐段宝岩杨东武杜敬利李申徐虎荣杨癸庚
Owner XIDIAN UNIV
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