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Conceptual Design of an Aerospace Vehicle Controller Using Axiomatic Theory

机译:基于公理的航天器控制器概念设计

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摘要

AEROSPACE systems are extremely involved with complexninterdependencies between the attendant subsystems, makingntheir design and engineering quite challenging. Requirements onnperformance, efficiency, economy, environmental effects, and issuesnof safety, reliability, ease of maintenance, and other factors, arenusually interlinked and may often be in mutual conflict. This has lednto the adoption of a systems engineering perspective to many aero-nspace design problems [1,2], and the development of processes,ntools, and methods broadly classed as system of systems engineeringn[3]. Yet, the design and development of aerospace systems, like anynother system design, must follow the natural course of ideate,nanalyze, check, and revise. The ideation phase is a creative processnwhere the designer must make a coherent problem statement thatnclearly captures the design requirements, and then come up with onenor more concepts that appear to meet the stated requirements. Eachnconceptmust be realized by one ormore designs (for example, vortexnlift conceptmay be realized by a canard or a strakeor a crankeddelta ornany other design), each of which must then be analyzed andnquantitative measures obtained that enable one to judge whether thendesign solves thegivenproblemand, if so,which among the designs isnthe best.Almost every device available to the designermay be seen tonbe a realization (inverse problem), analysis (modeling & simulation)nor a comparison (optimization) tool, with hardly any tool, if at all, tonhelp the designer in the conception phase. This is of concern,nespecially when the concept is innovative, not merely an improve-nment, but a radical departure from existing conceptual approaches tonthe problem.Admittedly, the conception process is highly subjective,ndepending on the creative powers of the designer and his/her ability tonintegrate knowledge in diverse disciplines. Yet, a systematic basis tonhelp the designer eliminate faulty concepts and narrowdown the fieldnto good designs will be of immense value in curtailing developmentntime and cost, and in yielding a superior product.
机译:AEROSPACE系统与相关子系统之间的复杂相互依赖关系极为复杂,因此其设计和工程难度很大。对性能,效率,经济,环境影响以及安全性,可靠性,易维护性和其他因素问题的要求通常是相互联系的,并且可能经常相互冲突。这导致对许多航空航天设计问题[1,2]采取系统工程的观点,并开发了广泛归类为系统工程系统的过程,工具和方法[3]。然而,与其他系统设计一样,航空系统的设计和开发也必须遵循构思,分析,检查和修改的自然过程。构想阶段是一个创造性的过程,在此过程中,设计师必须做出连贯的问题陈述,清楚地抓住设计要求,然后提出一个或多个似乎满足所述要求的概念。每个概念都必须通过一个或多个设计来实现(例如,涡旋升起的概念可以通过鸭嘴或曲柄或曲柄三角翼或其他设计来实现),然后必须对每个概念进行分析,并获得量化的量度,以使人们能够判断当时的设计是否解决了给定的问题,如果是的话,几乎所有设计人员可用的设备都可以看作是一种实现(逆问题),分析(建模和仿真)或比较(优化)工具,几乎没有任何工具可以帮助设计人员。设计师处于构思阶段。这是令人关注的,特别是当概念具有创新性时,不仅是改进,而且从根本上偏离了现有的概念方法,从而解决了这个问题。诚然,构想过程是高度主观的,取决于设计师及其创造力的创造力。她的能力使各种学科的知识融为一体。然而,系统的基础有助于设计师消除错误的概念并缩小生产范围,从而在减少开发时间和成本以及生产出优质产品方面具有巨大的价值。

著录项

  • 来源
    《Journal of Aircraft》 |2010年第6期|p.2149-2151|共3页
  • 作者

    N. Ananthkrishnan;

  • 作者单位

    Korea Advanced Institute of Science and Technology,Daejeon 305-701, Republic of Korea;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 23:06:14

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