微型卫星姿态确定和控制系统设计指南

2009 4th International Conference on Recent Advances in Space Technologies Pub Date : 2009-06-11 DOI:10.1109/RAST.2009.5158295

E. Oland, Alexander Aas, Tor Marius Steihaug, S. V. Mathisen, Frank R. Vedal

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引用次数: 1

摘要

本文提出了一种微型卫星姿态确定与控制系统的设计方法。它以ECSS文件为基础，并通过一个实际例子展示了ECSS标准如何应用于微型卫星项目。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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A design guide for attitude determination and control systems for picosatellites

In this paper we present a design methodology for attitude determination and control systems for picosatellites. It is based on the ECSS documentations and shows through a practical example how the ECSS standard can be applied to a picosatellite project.

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2009 4th International Conference on Recent Advances in Space Technologies

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