A multi-input multi-output adaptive feed-forward controller for vibration alleviation on a large blended wing body airliner-Reference-Cited by-同舟云学术

A multi-input multi-output adaptive feed-forward controller for vibration alleviation on a large blended wing body airliner

Published:2014-08 Issue:17 Volume:333 Page:3859-3880
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Wildschek A.,Bartosiewicz Z.,Mozyrska D.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference36 articles.

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5. J.F. Johnston, Accelerated development and flight evaluation of active controls concepts for subsonic transport aircraft, Load Alleviation/Extended Span Development and Flight Test, Vol. 1, NASA CR-159097, 1979, pp. 2–11.

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