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Title: Switching LPV control design with MDADT and its application to a morphing aircraft (English)
Author: He, Yong
Author: Li, Chunjuan
Author: Zhang, Weiguo
Author: Shi, Jingping
Author: Lü, Yongxi
Language: English
Journal: Kybernetika
ISSN: 0023-5954 (print)
ISSN: 1805-949X (online)
Volume: 52
Issue: 6
Year: 2016
Pages: 967-987
Summary lang: English
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Category: math
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Summary: In flight control of a morphing aircraft, the design objective and the dynamics may be different in its various configurations. To accommodate different performance goals in different sweep wing configurations, a novel switching strategy, mode dependent average dwell time (MDADT), is adopted to investigate the flight control of a morphing aircraft in its morphing phase. The switching signal used in this note is more general than the average dwell time (ADT), in which each mode has its own ADT. Under some simplified assumptions the control synthesis condition is formulated as a linear matrix optimization problem and a set of mode-dependent dynamic state feedback controllers are designed. Afterwards the proposed approach is applied to a morphing aircraft with a variable sweep wing to demonstrate its validity. (English)
Keyword: switching linear parameter-varying system
Keyword: flight control
Keyword: morphing aircraft
Keyword: mode dependent average dwell time
MSC: 93C95
MSC: 93D09
idZBL: Zbl 06707383
idMR: MR3607857
DOI: 10.14736/kyb-2016-6-0967
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Date available: 2017-02-13T11:48:34Z
Last updated: 2018-01-10
Stable URL: http://hdl.handle.net/10338.dmlcz/146000
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