Dynamic Optimum Design of Lunar Lander Considering Structural Parameter Uncertainty

被引：0
|
作者：
Chen Z.-Y. [1 ]
Liu L. [1 ]
Yue Z.-J. [1 ]
机构：
[1] Key Laboratory of Dynamics and Control of Flight Vehicle under Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, Beijing
来源：
Yuhang Xuebao/Journal of Astronautics | 2021年 / 42卷 / 12期
关键词：
Dynamic environment; Dynamic optimum design; Interval uncertainty; Lunar lander; Multi-domain substructure;
D O I：
10.3873/j.issn.1000-1328.2021.12.003
中图分类号：
学科分类号：
摘要：
To solve the problems of analysis time consuming and structural parameter uncertainty during the structural optimization of a lunar lander, a structural optimization framework of the lunar lander is proposed. Based on the multi-domain substructure synthesis method, the substructure model of the lunar lander is established and the dynamic analysis efficiency is improved. Based on the interval field method, the uncertain model of structural parameters is established, and the influencing uncertain parameters are obtained through the interval sensitivity analysis. To verify the framework, the structure of the solar wings and the mainbody bulkhead are optimized. The result shows that the framework can significantly improve the efficiency of the structural optimization. By comparing with the deterministic optimization results, it is verified that the structural optimization considering the structural uncertainty can improve the reliability of the analysis results. © 2021, Editorial Dept. of JA. All right reserved.
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页码：1502 / 1514
页数：12
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