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A SYSTEM FRAMEWORK FOR DESIGN ROBUSTNESS ANALYSIS OF HELICOPTER MID-LIFE UPGRADES

机译:直升机中生升级的设计稳健性分析的系统框架

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The global budget climate has laid restrictions on the design and development of new military aircraft to meet the demands of enhanced mission capabilities. To enhance mission capabilities, mid-life upgrade of in-service aircraft, with state-of-the-art mission systems onboard, is acknowledged as a cost-effective option. To facilitate the mid-life upgrade process, a "Decision Support System" is required to identify the state-of-the-art mission systems that will provide the enhanced mission capabilities. In this paper, a brief outline of An "Integrated Decision Support System" (IDSS) framework developed by a systems approach to identify mission systems is presented initially, followed by a detailed discussion on the development of 'Design Robustness Analysis' (DRA) sub-model. The DRA sub-model automates the robustness analysis of aircraft upgrade design against 'temporal uncertainties factors'.
机译:全球预算气候对新军用飞机的设计和开发奠定了限制,以满足加强特派团能力的需求。为提高特派团能力,船上最先进的使命系统的役飞机中生升级被认为是一种成本效益的选择。为方便中期升级过程,需要一个“决策支持系统”来确定将提供增强的使命能力的最先进的使命系统。在本文中,最初介绍了系统方法开发的“集成决策支持系统”(IDS)框架的简要概述,然后提出了关于“设计稳健性分析”(DRA)子的开发的详细讨论-模型。 DRA子模型自动化飞机升级设计对“时间不确定因素”的鲁棒性分析。

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