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Multi-level systems modeling and optimization for novel aircraft.

机译:新型飞机的多级系统建模和优化。

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摘要

This research combines the disciplines of system-of-systems (SoS) modeling, platform-based design, optimization and evolving design spaces to achieve a novel capability for designing solutions to key aeronautical mission challenges. A central innovation in this approach is the confluence of multi-level modeling (from sub-systems to the aircraft system to aeronautical system-of-systems) in a way that coordinates the appropriate problem formulations at each level and enables parametric search in design libraries for solutions that satisfy level-specific objectives. The work here addresses the topic of SoS optimization and discusses problem formulation, solution strategy, the need for new algorithms that address special features of this problem type, and also demonstrates these concepts using two example application problems - a surveillance UAV swarm problem, and the design of noise optimal aircraft and approach procedures.;This topic is critical since most new capabilities in aeronautics will be provided not just by a single air vehicle, but by aeronautical Systems of Systems (SoS). At the same time, many new aircraft concepts are pressing the boundaries of cyber-physical complexity through the myriad of dynamic and adaptive sub-systems that are rising up the TRL (Technology Readiness Level) scale. This compositional approach is envisioned to be active at three levels: validated sub-systems are integrated to form conceptual aircraft, which are further connected with others to perform a challenging mission capability at the SoS level. While these multiple levels represent layers of physical abstraction, each discipline is associated with tools of varying fidelity forming strata of 'analysis abstraction'. Further, the design (composition) will be guided by a suitable hierarchical complexity metric formulated for the management of complexity in both the problem (as part of the generative procedure and selection of fidelity level) and the product (i.e., is the mission best achieved via a large collection of interacting simple systems, or a relatively few highly capable, complex air vehicles). The vastly unexplored area of optimization in evolving design spaces will be studied and incorporated into the SoS optimization framework. We envision a framework that resembles a multi-level, mult-fidelity, multi-disciplinary assemblage of optimization problems.;The challenge is not simply one of scaling up to a new level (the SoS), but recognizing that the aircraft sub-systems and the integrated vehicle are now intensely cyber-physical, with hardware and software components interacting in complex ways that give rise to new and improved capabilities. The work presented here is a step closer to modeling the information flow that exists in realistic SoS optimization problems between sub-contractors, contractors and the SoS architect.
机译:这项研究结合了系统系统(SoS)建模,基于平台的设计,优化和不断发展的设计空间等学科,以实现为关键航空任务挑战设计解决方案的新颖能力。这种方法的核心创新是多级建模(从子系统到飞机系统再到航空系统的系统)的融合,其方式是在每个级别上协调适当的问题表述并允许在设计库中进行参数搜索用于满足特定级别目标的解决方案。此处的工作解决了SoS优化的主题,并讨论了问题的表述,解决方案策略,解决这种问题类型特殊功能的新算法的需求,并使用两个示例应用程序问题(监视无人机群问题和解决方案)演示了这些概念。最佳噪声飞机的设计和进近程序。该主题至关重要,因为航空领域的大多数新功能不仅将由单个飞行器提供,而且将由航空系统系统(SoS)提供。同时,许多新的飞机概念正通过无数动态和自适应子系统来推动网络物理复杂性的界限,这些子系统不断提高TRL(技术就绪水平)的规模。预计这种组合方法将在三个级别上发挥作用:将经过验证的子系统集成在一起,以形成概念飞机,然后将它们进一步与其他飞机连接起来,以在SoS级别上执行具有挑战性的任务能力。虽然这些多个级别代表物理抽象层,但每个学科都与形成“分析抽象”层次的各种保真度工具相关联。此外,设计(组成)将以适合管理问题(作为生成过程和保真度选择的一部分)和产品(即最佳实现任务的复杂性)的层次结构复杂性度量标准为指导通过大量相互作用的简单系统,或数量相对较少的高性能复杂航空器)。将研究不断变化的设计空间中尚未开发的优化领域,并将其纳入SoS优化框架中。我们构想了一个类似于多级,多保真,多学科的优化问题的框架;挑战不仅是将其扩展到新水平(SoS)的挑战之一,而且还要认识到飞机子系统如今,集成式汽车已成为高度网络物理设备,其硬件和软件组件以复杂的方式相互作用,从而产生了新的改进功能。本文介绍的工作距离建模分包商,承包商和SoS架构师之间的现实SoS优化问题中存在的信息流更近了一步。

著录项

  • 作者单位

    Purdue University.;

  • 授予单位 Purdue University.;
  • 学科 Engineering.;Aerospace engineering.
  • 学位 Ph.D.
  • 年度 2015
  • 页码 234 p.
  • 总页数 234
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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