A systematic method of smooth switching LPV controllers design for a morphing aircraft
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference33 articles.
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2. Analysis of transition stability for morphing aircraft;Seigler;J Guid Control Dyn,2009
3. Gain self-scheduled H∞ control for morphing aircraft in the wing transition process based on an LPV model;Yue;Chin J Aeronaut,2013
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