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Gaining System Design Knowledge by Systematic Design Space Exploration with Graph Based Design Languages

机译:通过基于图形设计语言的系统设计空间探索获得系统设计知识

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The conceptual design phase in the design of complex systems such as satellite propulsion systems heavily relies on an exploration of the feasible design space. This exploration requires both: topological changes in the potential system architecture and consistent parametrical changes in the dimensioning of the existing system components. Since advanced engineering design techniques nowadays advocate a model-based systems engineering (MBSE) approach, graph-based design languages which embed a superset of MBSE-features are consequently used in this work to systematically explore the feasible design space. Design languages allow the design knowledge to be represented, modeled and executed using model-based transformations and combine this among other features with constraint processing techniques. The execution of the design language shown for the satellite propulsion systems in this work yields topologically varied designs (i.e. the selection of a monergol, a diergol or a coldgas system) with consistent parameters. Based on an a posteriori performance analysis of the automatically generated system designs, novel system knowledge (most notably in form of so-called "topology change points ") can be gained and extracted from the original point cloud of numerical results.
机译:卫星推进系统等复杂系统设计中的概念设计阶段严重依赖于可行设计空间的探索。此探索需要:潜在系统架构中的拓扑变化以及现有系统组件的尺寸方面的一致参数变化。由于现在的先进的工程设计技术倡导基于模型的系统工程(MBSE)方法,因此在这项工作中使用了嵌入MBSE特征超集的基于图形的设计语言,以系统地探索可行的设计空间。设计语言允许使用基于模型的转换来表示,建模和执行的设计知识,并将其与其他功能与约束处理技术相结合。在该工作中针对卫星推进系统所示的设计语言产生拓扑变化的设计(即,选择一致的参数的单胞单根,Diergol或Coldgas系统)。基于对自动产生的系统设计的后验性能分析,可以从数值结果的原始点云获得和提取新的系统知识(最符合的形式,最值得注意的是所谓的“拓扑变化点”)。

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