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Automatic damping of vibrations of an airplane wing by internal control forces

โœ Scribed by V. I. Merkulov


Book ID
105001161
Publisher
SP MAIK Nauka/Interperiodica
Year
1981
Tongue
English
Weight
430 KB
Volume
21
Category
Article
ISSN
0021-8944

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## The vibrations of a rectangular plate are damped out by means of a combined open-closed-loop control mechanism. A functional involving the displacement, velocity and open-loop control Junction is minimized with respect to both the open-loop function and the displacement feedback parameter. The mi