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Proceedings Paper

A complete digital simulator for attitude control system design of nano-satellite
Author(s): Long Han; Xuecheng Jin; Xingxing Liu; Zengfu Wang
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Paper Abstract

We have designed a complete digital system simulator for the purpose of spacecraft attitude control. The simulator is composed of several modules including real-time sensor image generation module, processing module, attitude estimate module, and attitude control module. Furthermore, we have developed some virtual reality elements for future work. It will provide some capabilities in real-time data visualization. The experimental results show that this work can help us to validate our attitude sensing and control algorithm in the case without any physical instruments, and can provide usable data for future implementation.

Paper Details

Date Published: 4 January 2006
PDF: 5 pages
Proc. SPIE 5985, International Conference on Space Information Technology, 598503 (4 January 2006); doi: 10.1117/12.655643
Show Author Affiliations
Long Han, Univ. of Science and Technology of China (China)
Xuecheng Jin, Univ. of Science and Technology of China (China)
Xingxing Liu, Univ. of Science and Technology of China (China)
Zengfu Wang, Univ. of Science and Technology of China (China)


Published in SPIE Proceedings Vol. 5985:
International Conference on Space Information Technology
Cheng Wang; Shan Zhong; Xiulin Hu, Editor(s)

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