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Hierarchical modeling and robust synthesis for the preliminary design of large scale complex systems.

机译:大规模复杂系统的初步设计的层次建模和鲁棒综合。

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摘要

Large-scale complex systems are characterized by multiple interacting subsystems and the analysis of multiple disciplines. The design and development of such systems inevitably requires the resolution of multiple conflicting objectives. The size of complex systems, however, prohibits the development of comprehensive system models, and thus these systems must be partitioned into their constituent parts. Because simultaneous solution of individual subsystem models is often not manageable iteration is inevitable and often excessive.;In this dissertation these issues are addressed through the development of a method for hierarchical robust preliminary design exploration to facilitate concurrent system and subsystem design exploration, for the concurrent generation of robust system and subsystem specifications for the preliminary design of multi-level, multi-objective, large-scale complex systems. This method is developed through the integration and expansion of current design techniques: (1) Hierarchical partitioning and modeling techniques for partitioning large-scale complex systems into more tractable parts, and allowing integration of subproblems for system synthesis, (2) Statistical experimentation and approximation techniques for increasing both the efficiency and the comprehensiveness of preliminary design exploration, and (3) Noise modeling techniques for implementing robust preliminary design when approximate models are employed. The method developed and associated approaches are illustrated through their application to the preliminary design of a commercial turbofan turbine propulsion system; the turbofan system-level problem is partitioned into engine cycle and configuration design and a compressor module is integrated for more detailed subsystem-level design exploration, improving system evaluation.
机译:大型复杂系统的特征在于多个交互子系统和对多个学科的分析。这种系统的设计和开发不可避免地需要解决多个相互矛盾的目标。但是,复杂系统的规模限制了全面系统模型的开发,因此必须将这些系统划分为其组成部分。因为单个子系统模型的同时解决方案通常是不可管理的,所以迭代是不可避免的,而且经常是过多的。本文通过开发一种用于分层健壮的初步设计探索的方法来解决这些问题,以促进并发系统和子系统设计的探索,对于并发生成健壮的系统和子系统规范,以进行多层次,多目标,大型复杂系统的初步设计。通过集成和扩展当前设计技术来开发此方法:(1)分层划分和建模技术,用于将大型复杂系统划分为更易于处理的部分,并允许子问题集成以进行系统综合;(2)统计实验和近似用于提高初步设计探索的效率和综合性的技术;以及(3)当采用近似模型时用于实施可靠的初步设计的噪声建模技术。通过将其应用于商用涡扇涡轮推进系统的初步设计中,说明了所开发的方法和相关方法。涡轮风扇系统级问题分为发动机循环和配置设计,集成了压缩机模块以进行更详细的子系统级设计探索,从而改善了系统评估。

著录项

  • 作者

    Koch, Patrick Nathan.;

  • 作者单位

    Georgia Institute of Technology.;

  • 授予单位 Georgia Institute of Technology.;
  • 学科 Mechanical engineering.;Statistics.;Aerospace engineering.
  • 学位 Ph.D.
  • 年度 1998
  • 页码 435 p.
  • 总页数 435
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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