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Modeling the TPF Interferometer

机译:建模TPF干涉仪

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The Terrestrial Planet Finder interferometer design concepts are large and complex systems that must operate in environments that are impractical to reproduce in prefiight testing. The structurally-connected design is 36 meters long - longer than all but one thermal vacuum chamber in existence. The formation flying design will be comprised of up to five separate spacecraft, each with a sunshield over 15 meters on a side, and is designed to operate with formation sizes spanning 60-100 meters. System-level verification of the performance of the designs will rely on analytical modeling. The effort to model the many physical aspects of the designs under study is under way. This paper describes the program of modeling for the TPF-I concepts. The program includes a number of types of models, such as the standard stand-alone optics, thermal, and structural models, as well as an end-to-end performance model of the project system called the Observatory Simulation. Aspects of each model are discussed including the purpose, methods of implementation (software applications), and approaches to validation. Program-level considerations (such as model-to-model integration and configuration management) are also discussed. Given that there are at least seven different organizations contributing to model developments and more than twenty separate models, these are special challenges.
机译:地面行星发现者干涉仪设计概念是大型且复杂的系统,必须在以前视测试中重现的环境不切实际的环境中运行。结构连接的设计长36米长,而不是一个热真空室的存在。形成飞行设计将由最多五个独立的航天器组成,每个航天器均有超过15米的遮阳板,旨在与跨越60-100米的地层尺寸运行。系统级验证设计性能将依赖于分析建模。努力建模研究的许多物理方面正在进行中。本文介绍了TPF-I概念的建模程序。该程序包括许多类型的模型,例如标准独立光学,热和结构模型,以及项目系统的端到端性能模型,称为天文台模拟。讨论了每个模型的各个方面,包括目的,实现方法(软件应用程序),以及验证方法。还讨论了程序级别注意事项(例如模型到模型集成和配置管理)。鉴于至少有七种不同的组织有助于模型发展和超过二十个独立型号,这些是特别的挑战。

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