Open AccessHigh-Frequency Vibration Control of Rotating Beam Based on Trailing-edge Flap
Author(s) -
Wang Jian,
Shanyao Li,
Changle Sun,
Tingrui Liu
Publication year - 2022
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/2173/1/012050
Subject(s) - trailing edge , control theory (sociology) , aeroelasticity , robustness (evolution) , vibration , robust control , vibration control , beam (structure) , displacement (psychology) , control system , engineering , computer science , structural engineering , aerodynamics , physics , acoustics , control (management) , psychology , biochemistry , chemistry , electrical engineering , artificial intelligence , gene , aerospace engineering , psychotherapist
This study is to investigate an active control method, based on trailing-edge flap, in high-frequency vibration control of rotating blade beam. The structure is modeled as composite blade beam with circumferentially asymmetric stiffness configuration, which is based on analysis of the elastic flap-wise/twist displacements and incorporates the angle control of trailing-edge flap driven by a stepping motor. Aerodynamic expressions are based on a novel quasi-steady model suitable for trailing-edge flap. Based on a strip theory, the multi-body dynamic aeroelastic system is analyzed and solved. The active control is realized by Hœ algorithm using linear matrix inequality (LMI) design. This study is to investigate time-domain stability analysis and robust control method, realize displacement response analysis and robust performance analysis, and input signal display of trailing-edge flap angle. The optimization mechanism of LMI is to optimize uncertain robust performance parameters based on the selection of robust control parameters, so that the controlled displacement and control input are kept within reasonable ranges. The reliability and robustness of H» control algorithm based on LMI are verified by comparisons of the results of high-frequency vibration control using different robust performance parameters.