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  • 期刊=Transactions of Nanjing University of Aeronautics and Astronauticsx
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Dynamic Modeling and Adaptive Fast Nonsingular Terminal Sliding Mode Control for Satellite with Double Rotary Payloads被引量:1
《Transactions of Nanjing University of Aeronautics and Astronautics》2016年第3期310-318,共9页Xu Chen Lu Yuping Yao Keming Liu Yanbin Xiao Dibo 
supported by the National Natural Science Foundation of China(No.91016017);the Funding of Jiangsu Innovation Program for Graduate Education (No. CXZZ12_0160);the Natural Science Foundation of Jiangsu Province of China(No.BK20130234);the Changzhou Sci.& Tech.Program (CE20145056)
A robust attitude control methodology is proposed for satellite system with double rotary payloads. The dynamic model is built by the Newton-Euler method and then the dynamic interconneetion between satellite's main ...
关键词:satellite with double rotary payloads multi-rigid-body system sliding mode control disturbance observers attitude control 
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