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A method for concept and technology exploration of aerospace architectures.

机译:一种用于航空航天体系结构的概念和技术探索的方法。

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摘要

This dissertation presents the development of a new concept and technology exploration methodology for aerospace architectures. The methodology is based on modeling the design space by a graph, and optimizing the graph using Ant Colony Optimization. The results show that the proposed design methodology can explore more efficiently the concept and technology space of a launch vehicle architecture than traditional optimization approaches such as Genetic Algorithm and Simulated Annealing.; The purpose of the method is to introduce quantitative and simultaneous exploration of concept and technology alternatives during the early phases of conceptual design. To achieve this goal, technical challenges such as expanding the size of the design space, exploring more efficiently the design options, and simultaneously considering technologies and concepts are overcome.; The total number of design alternatives grows factorially with the number of concepts in the design space. Under these circumstances, the design space is difficult to explore in its totality. Considering more alternatives has been the focus of several researchers, using Genetic Algorithms and Simulated Annealing. The large number of incompatibilities between alternatives, however, limits these optimization algorithms and reduces the number of concepts or technologies that can be considered.; To address these problems, a concept and technology selection methodology is developed. The methodology proposes a way to automatically generate aerospace architectures, and to model concept and technology incompatibilities by means of a graph. In conjunction with this new modeling approach, a graph-based stochastic optimization algorithm is used to efficiently explore the design space. This design methodology is applied to the simultaneous concept and technology exploration of an expendable launch vehicle architecture.; This study demonstrates that the consideration of more design alternatives can help design engineers to make more informed decisions during the concept and technology selection process. Moreover, the simultaneous exploration of concepts and technologies has the potential to identify a different set of solutions than the standard approach where the technologies are explored after the concepts have initially been selected.
机译:本文提出了一种新的航空航天概念和技术探索方法。该方法基于通过图形对设计空间进行建模,并使用蚁群优化对图形进行优化。结果表明,与传统的优化方法如遗传算法和模拟退火算法相比,所提出的设计方法可以更有效地探索运载火箭架构的概念和技术空间。该方法的目的是在概念设计的早期阶段引入对概念和技术替代方案的定量和同步探索。为了实现这一目标,克服了技术难题,例如扩大设计空间的大小,更有效地探索设计方案以及同时考虑技术和概念。设计替代方案的总数随着设计空间中概念的数量而析因地增长。在这种情况下,很难对设计空间进行整体探索。使用遗传算法和模拟退火法,考虑更多替代方法已成为几位研究人员的重点。但是,备选方案之间存在大量不兼容性,这限制了这些优化算法并减少了可以考虑的概念或技术的数量。为了解决这些问题,开发了一种概念和技术选择方法。该方法提出了一种自动生成航空航天体系结构,并通过图形对概念和技术不兼容进行建模的方法。结合这种新的建模方法,使用基于图的随机优化算法来有效地探索设计空间。这种设计方法适用于消耗性运载火箭架构的同步概念和技术探索。这项研究表明,更多设计替代方案的考虑可以帮助设计工程师在概念和技术选择过程中做出更明智的决策。此外,与概念和技术同时进行探索相比,在最初选择概念之后对技术进行探索的标准方法,有可能找到一套不同的解决方案。

著录项

  • 作者

    Villeneuve, Frederic.;

  • 作者单位

    Georgia Institute of Technology.;

  • 授予单位 Georgia Institute of Technology.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2007
  • 页码 252 p.
  • 总页数 252
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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