Spacecraft attitude tracking control under actuator magnitude deviation and misalignment
Authors:
- Qinglei HuQHQinglei Hu
- Bo LiBLBo Li
- Xing HuoXHXing Huo
- Zhong ShiZSZhong Shi
- 1 July 2013
- journal article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 28 (1) , 266-280
Abstract
No abstract availableKeywords
Funding Information
- Program for New Century Excellent Talents in University (NCET-11-0801)
- Heilongjiang Youth Development Foundation (QC2012C024)
- National Natural Science Foundation of China (61273175, 61174200, 61004072)
- Fundamental Research Funds for the Central Universities (HIT.BRETIII.201212)
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