Decentralized active damping control for aeroelastic morphing wing

被引：1
|
作者：
Svoboda, Filip [1 ]
Hengster-Movric, Kristian [1 ]
Hromcik, Martin [1 ]
Sika, Zbynek [2 ]
机构：
[1] Czech Tech Univ, Fac Elect Engn, Karlovo Namesti 13, Prague 12135, Czech Republic
[2] Czech Tech Univ, Fac Mech Engn, Tech 4, Prague 16000, Czech Republic
来源：
AEROSPACE SCIENCE AND TECHNOLOGY | 2023年 / 139卷
关键词：
Decentralized control; Morphing wing; Aeroelasticity; Linear matrix inequalities; MULTIAGENT SYSTEMS; STATE-FEEDBACK; DESIGN; AIRCRAFT; SYNCHRONIZATION; CONSENSUS; NETWORKS;
D O I：
10.1016/j.ast.2023.108415
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper introduces a novel decentralized control design procedure for an aeroelastic morphing wing. The control goal is active damping of this flexible system. The model is developed as a multi-agent system with inherent interconnections between the agents. The control system then takes advantage of the model structure and interconnections rather than relying on the entire system's model. This brings benefits, especially with a growing number of agents where the control design dimension remains low. Therefore, the proposed control design is especially suitable for morphing wings with a large number of actuation points. The result is presented in the Linear Matrix Inequalities (LMIs) form. A numerical example shows the application of the proposed algorithm. & COPY; 2023 Elsevier Masson SAS. All rights reserved.
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页数：10
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