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4 January 2006 A complete digital simulator for attitude control system design of nano-satellite
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Proceedings Volume 5985, International Conference on Space Information Technology; 598503 (2006) https://doi.org/10.1117/12.655643
Event: International Conference on Space information Technology, 2005, Wuhan, China
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.
© (2006) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Long Han, Xuecheng Jin, Xingxing Liu, and Zengfu Wang "A complete digital simulator for attitude control system design of nano-satellite", Proc. SPIE 5985, International Conference on Space Information Technology, 598503 (4 January 2006); https://doi.org/10.1117/12.655643
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