Optimizing accuracy of a parabolic cylindrical deployable antenna mechanism based on stiffness analysis
Accuracy of the fitted surface is of great importance to the performance of deployable antennas utilized in space. This paper proposes a stiffness analysis based fitting accuracy optimization method for achieving the optimal parameters of the parabolic cylindrical deployable antenna mechanism. The s...
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| Published in | Chinese journal of aeronautics Vol. 33; no. 5; pp. 1562 - 1572 |
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| Main Authors | , , |
| Format | Journal Article |
| Language | English |
| Published |
Elsevier Ltd
01.05.2020
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| Subjects | |
| Online Access | Get full text |
| ISSN | 1000-9361 |
| DOI | 10.1016/j.cja.2019.05.017 |
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| Abstract | Accuracy of the fitted surface is of great importance to the performance of deployable antennas utilized in space. This paper proposes a stiffness analysis based fitting accuracy optimization method for achieving the optimal parameters of the parabolic cylindrical deployable antenna mechanism. The stiffness matrix of the proposed cylindrical antenna mechanism is established by assembling the stiffness of beams and tension cables. Structural deformations of the mechanism are calculated where the tensioned cable is substituted by a 2-node truss element and an equivalent force acting on the joint. Consideration of the tensity of tension cables, namely tensioned or slack, is transformed into a typical linear complementarity problem. Comparison between structural deformations of the mechanism fixed at different points is performed. Sensitivities of the geometric and structural parameters on fitting accuracy are investigated. Influence of force of the driven cable on structural deformations of antenna operated in different orbits is conducted. A fitting optimization method is proposed to minimize the structural deformations subject to constraints on volume and mass. Simulation result shows that the fitting accuracy of the antenna mechanism is improved significantly through the optimization. The proposed method can be utilized for the optimal design of other deployable mechanisms constructed by joining rigid links. |
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| AbstractList | Accuracy of the fitted surface is of great importance to the performance of deployable antennas utilized in space. This paper proposes a stiffness analysis based fitting accuracy optimization method for achieving the optimal parameters of the parabolic cylindrical deployable antenna mechanism. The stiffness matrix of the proposed cylindrical antenna mechanism is established by assembling the stiffness of beams and tension cables. Structural deformations of the mechanism are calculated where the tensioned cable is substituted by a 2-node truss element and an equivalent force acting on the joint. Consideration of the tensity of tension cables, namely tensioned or slack, is transformed into a typical linear complementarity problem. Comparison between structural deformations of the mechanism fixed at different points is performed. Sensitivities of the geometric and structural parameters on fitting accuracy are investigated. Influence of force of the driven cable on structural deformations of antenna operated in different orbits is conducted. A fitting optimization method is proposed to minimize the structural deformations subject to constraints on volume and mass. Simulation result shows that the fitting accuracy of the antenna mechanism is improved significantly through the optimization. The proposed method can be utilized for the optimal design of other deployable mechanisms constructed by joining rigid links. |
| Author | XIAO, Hang LYU, Shengnan DING, Xilun |
| Author_xml | – sequence: 1 givenname: Hang surname: XIAO fullname: XIAO, Hang – sequence: 2 givenname: Shengnan surname: LYU fullname: LYU, Shengnan email: shengnan_lyu@buaa.edu.cn – sequence: 3 givenname: Xilun surname: DING fullname: DING, Xilun |
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| Keywords | Cable-driven Stiffness analysis Accuracy analysis Optimization Deployable antennas |
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| Snippet | Accuracy of the fitted surface is of great importance to the performance of deployable antennas utilized in space. This paper proposes a stiffness analysis... |
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| SubjectTerms | Accuracy analysis Cable-driven Deployable antennas Optimization Stiffness analysis |
| Title | Optimizing accuracy of a parabolic cylindrical deployable antenna mechanism based on stiffness analysis |
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