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A Constraint Based Approach for Building Operationally Responsive Space Satellites

机译:基于约束的制造运行响应空间卫星的方法

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The Operationally Responsive Space program requires flexible and responsive satellites to meet their user's needs. Traditional satellite design methods are typically iterative processes that optimize individual components, subsystems, and ultimately the entire satellite. This study focuses on developing a new approach for creating Responsive Satellites from Plug-and-Play components. The aim is to create an approach that quickly evaluates a wide variety of possible satellite configurations and identifies the best configurations that meet the user's needs and constraints. Satellite configurations are created by matching locations on the satellite structure with Plug-and-Play components. Various constraints are derived from the user's inputs at different levels of the configuration process. As the user provides more information related to Plug-and-Play satellite, additional constraints can be applied to reduce the number of Plug-and-Play satellite configurations resulting in manageable numbers of configurations from which the user can ultimately select the final configuration.
机译:操作响应性的空间计划需要灵活和响应卫星来满足其用户的需求。传统的卫星设计方法通常是优化各个组件,子系统和最终整个卫星的迭代过程。本研究侧重于开发一种从即插即用组件创建响应卫星的新方法。目的是创建一种快速评估各种可能的卫星配置的方法,并识别满足用户需求和约束的最佳配置。通过使用即插即用组件匹配卫星结构上的位置来创建卫星配置。各种约束来自用户的配置过程的不同级别的输入。由于用户提供了与即插即用卫星相关的更多信息,因此可以应用附加约束以减少即插即用的卫星配置的数量,导致用户最终可以选择最终配置的可管理数量的配置。

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