Flutter Control of a Two-dimensional Airfoil based on Adaptive Dynamic Programming

The severe aeroelastic vibrations can lead to structural damage and threaten the flight safety. It is an important topic to develop active controllers for aeroelastic stabilization and flutter suppression. The traditional control methods need the clearly established mathematic model, whereas establi...

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Veröffentlicht in:	IOP conference series. Materials Science and Engineering Jg. 531; H. 1; S. 12033 - 12040
Hauptverfasser:	Jia, Su, Sun, Jian Qiao, Ding, Qian
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Bristol IOP Publishing 01.09.2019
Schlagworte:	Adaptive control Aeroelasticity Airfoils Algorithms Control methods Control surfaces Dynamic models Dynamic programming Flight safety Flutter Nonlinearity Structural damage Vibration
ISSN:	1757-8981, 1757-899X
Online-Zugang:	Volltext
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