In this paper, a composite domain topology optimization (CDTO) method is proposed to control the distribution of different amount of material in the design sub-domain of structure.
提出一种复合域拓扑优化方法以控制结构设计子域的不同材料数量分布。
For the multidisciplinary design optimization (MDO) of spacecraft with sub-vehicles, system mission requirements and disciplinary coupling relations are analyzed.
针对带子星航天器总体参数多学科设计优化(MDO)问题,进行系统任务分析和学科耦合关系分析。
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