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首页> 外文期刊>Aerospace and Electronic Systems Magazine, IEEE >Revolutionary design meets spacecraft reality: Lessons learned
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Revolutionary design meets spacecraft reality: Lessons learned

机译:革命性设计满足航天器现实:经验教训

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摘要

The Plug and Play Satellite (PnPSat) Program, initiated by the Air Force Research Laboratory in Albuquerque, New Mexico, is both a testbed for innovative spacecraft components and integration concepts, and a fully functional spacecraft with the first Flight Unit rapidly approaching night-readiness. While the intent of the PnPSat Program is to prove technologies and implement processes that allow rapid integration and test of flight-ready units, the integration of the first PnPSat flight article has not been without more traditional platform integration challenges. Design_Net Engineering (D_Net) has been tasked with supplying both hardware and systems expertise to develop most of the power sub-system components for PnPSat. We have successfully developed, delivered, and integrated a Solar Array Controller (SAC) and an Energy Storage Module (ESM) that provide hardware and software interfaces necessary to effectively enable solar power acquisition and management on the PnPSat spacecraft. The lessons learned along the path to successful integration and test will be of value to anyone else developing hardware and firmware destined for the PnPSat architecture. The PnPSat program paradigm is based on a readily available collection of hardware components and their associated embedded software interfaces (on-shelf “at the depot”) that can be assembled in a variety of configurations on a standard spacecraft structure, providing a fully configured and tested, flight-ready spacecraft within a matter of days following call-up. The principal challenge facing the Power Subsystem developer under these unique design constraints is to deliver a system that does not simply meet a point design spec, but rather one that includes component modules capable of supporting a wide range of future mission requirements, while also fitting the form factor and interface architecture dictated by the need for component relocateability; and while capable of reliable operation in such -n-na distributed power architecture. Design_Net''s hardware implementations satisfy all functional and performance requirements imposed by all projected PoPSat mission needs, while maintaining the ability to be placed anywhere on or in the spacecraft.
机译:由新墨西哥州阿尔伯克基市空军研究实验室发起的即插即用卫星(PnPSat)计划既是创新型航天器组件和集成概念的试验台,也是功能齐全的航天器,第一个飞行单元迅速接近夜间准备状态。虽然PnPSat计划的目的是证明技术和实施过程,以允许快速集成和测试飞行就绪部队,但第一篇PnPSat飞行文章的集成并非没有传统的平台集成挑战。 Design_Net Engineering(D_Net)的任务是提供硬件和系统专业知识,以开发用于PnPSat的大多数电源子系统组件。我们已成功开发,交付并集成了太阳能电池阵列控制器(SAC)和储能模块(ESM),它们提供了有效启用PnPSat航天器上的太阳能采集和管理所必需的硬件和软件接口。在成功进行集成和测试的过程中所汲取的经验教训对于开发用于PnPSat体系结构的硬件和固件的任何其他人都是有价值的。 PnPSat程序范式基于硬件组件及其关联的嵌入式软件接口(现成的“仓库”)的随时可用集合,这些接口可以以各种配置组装在标准航天器结构上,从而提供完整的配置和召唤后几天之内就可以进行飞行测试,并且可以飞行。在这些独特的设计约束下,Power Subsystem开发人员面临的主要挑战是提供一种系统,该系统不仅要满足点设计规范,还需要包含能够支持各种未来任务要求的组件模块,同时还要满足这些要求。组件可重定位的需要决定了外形尺寸和接口架构;并且能够在这种-n-na分布式电源架构中可靠运行。 Design_Net的硬件实现满足了所有预计的PoPSat任务需求所提出的所有功能和性能要求,同时保持了将其放置在航天器上或航天器中任何位置的能力。

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