Paper
20 September 2022 Optimal design of deployment mechanism of spaceborne umbrella deployable antenna
Tingting Liu, Yue Hua, Guohui Chen, Tian Shi
Author Affiliations +
Proceedings Volume 12261, International Conference on Mechanical Design and Simulation (MDS 2022); 122611J (2022) https://doi.org/10.1117/12.2638892
Event: Second International Conference on Mechanical Design and Simulation (MDS 2022), 2022, Wuhan, China
Abstract
In this paper, the deployment mechanism of the spaceborne umbrella deployable antenna is taken as the research object. The working principle of the deployment mechanism is introduced, and the equation of motion of the deployment mechanism is obtained by using the analytical method. Combined with the structural parameters of the moving parts of the antenna deployment mechanism, the motion law of the key parts of the deployment mechanism in the process of antenna deployment is obtained. Through the force analysis of the deployment mechanism, the structure optimization model of the deployment mechanism is established, which takes the structural parameters of the deployment mechanism as the design variables and the minimum driving force as the objective. Through the ergodic method, the optimized structural parameters of the deployment mechanism are obtained. The maximum driving force of the optimized deployment mechanism is 30% lower than that before optimization, and the optimization effect is remarkable.
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Tingting Liu, Yue Hua, Guohui Chen, and Tian Shi "Optimal design of deployment mechanism of spaceborne umbrella deployable antenna", Proc. SPIE 12261, International Conference on Mechanical Design and Simulation (MDS 2022), 122611J (20 September 2022); https://doi.org/10.1117/12.2638892
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KEYWORDS
Antennas

Optimization (mathematics)

Analytical research

Resistance

Reflectors

Motion analysis

Motion models

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