Adaptive control design for the aeroelastic wing

被引：0
|
作者：
Svoboda, Filip [1 ]
Hromcik, Martin [1 ]
Sika, Zbynek [1 ]
机构：
[1] Czech Tech Univ, Fac Elect Engn, Prague, Czech Republic
来源：
PROCESS CONTROL '21 - PROCEEDING OF THE 2021 23RD INTERNATIONAL CONFERENCE ON PROCESS CONTROL (PC) | 2021年
关键词：
aeroelasticity; flutter; H-infinity design; LPV system; adaptive control; FLUTTER SUPPRESSION; SYSTEM;
D O I：
10.1109/PC52310.2021.9447451
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The design of adaptive control for an aeroelastic wing using structured H-infinity synthesis is presented in this paper. The algorithm uses a polynomial interpolation of controller parameters for a wide airspeed range. The structure of control law is fixed, with its parameters determined for a given airspeed range. We demonstrate the possibilities of such a controller for active flutter suppression on the linear parameter-varying (LPV) servoaeroelastic wing model with two ailerons.
引用
收藏
页码：225 / 228
页数：4
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