Synthesis and Flight Test of Automatic Landing Controller Using Quantitative Feedback Theory

Published 2016 View Full Article

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Title
Synthesis and Flight Test of Automatic Landing Controller Using Quantitative Feedback Theory
Authors
Keywords
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Journal
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
Volume 39, Issue 9, Pages 1994-2010
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2016-07-21
DOI
10.2514/1.g001758
References
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