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[IEEE 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics (ISSCAA) - Harbin, China (2010.06.8-2010.06.10)] 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics - A two-step LMI approach to robust dynamic output feedback control for the MIMO aircraft model F-18

✍ Scribed by Song, Lei; Yang, Jianying

Book ID: 115543938
Publisher: IEEE
Year: 2010
Weight: 691 KB
Volume: 0
Category: Article
ISBN: 1424460433
DOI: 10.1109/isscaa.2010.5632873

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