微型卫星低成本容错机载计算机的设计与实现

Shiqiang Tian, Zuobiao Yin, Jian Yan, Xuming Liu
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引用次数: 1

摘要

近年来,微卫星作为航天领域的重要前沿,在各种面向空间的任务中得到了广泛的应用。在各种机载组件中,机载计算机(OBC)负责许多任务,如命令和数据处理,通信和有效载荷管理。然而,由于微型卫星资源有限,OBC既要满足性能优良、可靠性高的要求,又要控制在适当的功耗和成本范围内。本文的目的是提出一种开发低成本、低功耗、可靠的微型卫星OBC系统的解决方案。该系统基于商用现货(COTS)组件和Linux操作系统。此外,针对恶劣的空间环境,引入了一套容错策略,提高了OBC的可靠性。最后,给出了分析和测试结果,说明了所提出的OBC系统相对低成本、低功耗和高可靠性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design and implementation of a low-cost fault-tolerant on-board computer for micro-satellite
In recent years, as an important frontier of astronautics, micro-satellites have been widely used for various space-oriented missions. During various on-board components, the on-board computer (OBC) is essential to take charge of many tasks such as command and data handing, communication and payload management. However, the resources on micro-satellites are so limited that the OBC should not only meet the requirements of excellent performance and high reliability, but also be in proper power consumption and cost. The purpose of this paper is to present a solution for developing a low-cost, low power consumption and reliable OBC system for micro-satellites. The proposed system is based on commercial-off-the-shelf (COTS) components and Linux operating system. Besides, considering the harsh space environment, a set of fault tolerant strategies are introduced to improve the reliability of the OBC. Finally, the analysis and test results are provided to illustrate the relatively low-cost, low power consumption and high reliability of the proposed OBC system.
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