Smooth finite-time fault-tolerant attitude tracking control for rigid spacecraft
Authors:
- Qinglei HuQHQinglei Hu
- Xiaodong ShaoXSXiaodong Shao
- 1 August 2016
- journal article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 55, 144-157
Abstract
No abstract availableFunding Information
- National Natural Science Foundation of China (61273175, 61522301)
- Program for New Century Excellent Talents in University (NCET-11-0801)
- Heilongjiang Province Science Foundation for Youths (QC2012C024)
- Research Fund for Doctoral Program of Higher Education of China (20132302110028)
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