Switching LPV control design with MDADT and its application to a morphing aircraft

Yong He; Chunjuan Li; Weiguo Zhang; Jingping Shi; Yongxi Lü

Kybernetika (2016)

  • Volume: 52, Issue: 6, page 967-987
  • ISSN: 0023-5954

Abstract

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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.

How to cite

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He, Yong, et al. "Switching LPV control design with MDADT and its application to a morphing aircraft." Kybernetika 52.6 (2016): 967-987. <http://eudml.org/doc/287920>.

@article{He2016,
abstract = {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.},
author = {He, Yong, Li, Chunjuan, Zhang, Weiguo, Shi, Jingping, Lü, Yongxi},
journal = {Kybernetika},
keywords = {switching linear parameter-varying system; flight control; morphing aircraft; mode dependent average dwell time},
language = {eng},
number = {6},
pages = {967-987},
publisher = {Institute of Information Theory and Automation AS CR},
title = {Switching LPV control design with MDADT and its application to a morphing aircraft},
url = {http://eudml.org/doc/287920},
volume = {52},
year = {2016},
}

TY - JOUR
AU - He, Yong
AU - Li, Chunjuan
AU - Zhang, Weiguo
AU - Shi, Jingping
AU - Lü, Yongxi
TI - Switching LPV control design with MDADT and its application to a morphing aircraft
JO - Kybernetika
PY - 2016
PB - Institute of Information Theory and Automation AS CR
VL - 52
IS - 6
SP - 967
EP - 987
AB - 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.
LA - eng
KW - switching linear parameter-varying system; flight control; morphing aircraft; mode dependent average dwell time
UR - http://eudml.org/doc/287920
ER -

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