Quaternion-based adaptive terminal sliding mode control for spacecraft attitude tracking - researchr publication authors

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Shunan Wu, Guoqiang Wu, Shujun Tan, Zhigang Wu. Quaternion-based adaptive terminal sliding mode control for spacecraft attitude tracking. In 10th IEEE International Conference on Control and Automation, ICCA 2013, Hangzhou, China, June 12-14, 2013. pages 913-917, IEEE, 2013. [doi]

This author has not been identified. Look up 'Shunan Wu' in GoogleThis author has not been identified. Look up 'Guoqiang Wu' in GoogleThis author has not been identified. Look up 'Shujun Tan' in GoogleThis author has not been identified. Look up 'Zhigang Wu' in Google

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