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DEVELOPMENT OF A METHODOLOGY TO OPTIMALLY SELECT SUBSYSTEMS FOR SUBSEQUENT INTEGRATION INTO HELICOPTER SYSTEMS

机译:为后续集成到直升机系统中的最优选择子系统的方法开发

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A systems engineering methodology and model are presented for selecting subsystems and interfaces that meet technical and budgetary requirements, with specific emphasis on helicopter development. The methodology expresses the problem of subsystem selection in terms of a graph theoretic model, conditioned for optimization based on enterprise goals. The model is visually represented as a network flow where nodes represent subsystems, and arcs represent subsystem interfaces. The interface parameters consist not of physical and functional relationships, but instead represent cost, schedule, technical performance, and risk. Those key technical and budgetary attributes are drawn into the model as optimization objectives. Mathematical formulation describes the complex system objectives, constraints, variables, and dependencies in terms of a multi-objective optimization model where parameters important to the product integration scheme are simultaneously quantified as part of the system model. The solution set is a Pareto optimal list of alternative subsystems ranked in order of preference, allowing the developer a selection of subsystem combinations to meet technical performance requirements and satisfy budgetary goals.
机译:提出了一种系统工程方法论和模型,用于选择满足技术和预算要求的子系统和接口,特别侧重于直升机的开发。该方法用图论模型表达了子系统选择的问题,该模型基于企业目标进行了优化。该模型在视觉上表示为网络流,其中节点表示子系统,弧表示子系统接口。接口参数不包含物理和功能关系,而是代表成本,进度,技术性能和风险。这些关键的技术和预算属性被作为优化目标纳入模型。数学公式以多目标优化模型的形式描述了复杂的系统目标,约束,变量和依赖性,其中对产品集成方案重要的参数同时作为系统模型的一部分进行了量化。解决方案集是按优先顺序排列的替代子系统的帕累托最优列表,允许开发人员选择子系统组合,以满足技术性能要求并满足预算目标。

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