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SYSTEMS CONCURRENT ENGINEERING PICO-SATELLITES

机译:系统同步工程微型卫星

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This paper aims to describe a template containing all elements for systems engineering pico-satellites. Thetemplate aims to be generic for accomplishing the needs of university Cubesats development programs and to bereused by such programs. It is implemented in a commercial systems engineering software environment calledCradle ? and it was developed based on the experience of the University of Wurzburg, in Germany, where threesatellites of the UWE series have already been developed since 2005. It covers: mission definition which includesstakeholder analysis, concept of operations and operational concept architecture; system requirements analysis;system architecture that shows the functional structure and behavior of the system and systems elements and thephysical or implementation architecture of the system; the detailed design that provides the system componentspecifications; the plans for all life cycle processes of the system such as development, manufacturing, assembly,integration, testing, launching, operations and disposal. The template was developed with a life cycle processperspective, using concurrent engineering principles of anticipation of life cycle process requirements to the earlystages of product development. Therefore, the models constructed in the template capture the satellite in everyscenario along its life cycle. For example, the models describe the context of the satellite during operations but alsoduring thermal vacuum testing or during launch and launch preparation. The template aims to be an instrument forteaching and learning space systems engineering and to ease the documentation burden necessary to develop a spaceproduct. It offers a solution to university satellite programs where, in general, the students do not have enoughsystems engineering background nor the university has a professional structure for systems engineering and projectmanagement. The paper also provides an example of the use of the template with the Cubesats currently underdevelopment in Brazil at INPE (Brazilian Institute for Space Research) and ITA (Aeronautics Institute ofTechnology).
机译:本文旨在描述一个模板,其中包含用于系统工程微卫星的所有元素。这 该模板旨在通用以满足大学Cubesats开发计划的需求,并成为 由此类程序重用。它是在称为的商业系统工程软件环境中实现的 摇篮?它是根据德国维尔茨堡大学的经验开发的,其中三个 自2005年以来,已经开发了UWE系列卫星。它涵盖:任务定义,其中包括 利益相关者分析,运营概念和运营概念架构;系统需求分析; 系统架构,显示系统的功能结构和行为以及系统元素和 系统的物理或实现体系结构;提供系统组件的详细设计 规格;系统所有生命周期过程的计划,例如开发,制造,组装, 集成,测试,发射,运营和处置。该模板是通过生命周期过程开发的 观点,使用并发工程原理来预期生命周期过程的早期需求 产品开发阶段。因此,模板中构建的模型会捕获每个 整个生命周期中的场景。例如,这些模型不仅描述了运营期间卫星的情况,而且还描​​述了 在热真空测试期间或在发射和发射准备期间。该模板旨在成为 教学和学习太空系统工程,并减轻开发太空所需的文档负担 产品。它为通常情况下学生不够的大学卫星课程提供了解决方案 系统工程背景,大学也没有专业的系统工程和项目架构 管理。本文还提供了将模板与当前使用的Cubesats一起使用的示例 巴西INPE(巴西空间研究所)和ITA(航空研究所 技术)。

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