Finite-Time Output Feedback Attitude Tracking Control for Rigid Spacecraft

Published 2014 View Full Article

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Title
Finite-Time Output Feedback Attitude Tracking Control for Rigid Spacecraft
Authors
Keywords
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Journal
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY
Volume 22, Issue 1, Pages 338-345
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Online
2014-01-04
DOI
10.1109/tcst.2013.2246836

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