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Adaptive Back-Stepping Sliding Mode Attitude Tracking of Rigid Spacecraft with disturbances}%uthorCHN{张三丰ffil{1},李四ffil{2} |
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LU Kunfeng,XIA Yuanqing *
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School of Automation, Beijing Institute of Technology
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*Correspondence author |
#Submitted by |
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Subject: |
Funding:
National Basic Research Program of China (973 Program) (No.2012CB720000), Beijing Municipal Natural Science Foundation(No.4102053, 4101001), the Ph.D. Programs Foundation of Ministry of Education of China(No.20091101110023, 20111101110012), National Natural Science Foundation of China(No.61225015, 60974011) |
Opened online:28 December 2012 |
Accepted by:
none |
Citation: LU Kunfeng,XIA Yuanqing.Adaptive Back-Stepping Sliding Mode Attitude Tracking of Rigid Spacecraft with disturbances}%uthorCHN{张三丰ffil{1},李四ffil{2}[OL]. [28 December 2012] http://en.paper.edu.cn/en_releasepaper/content/4502987 |
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