Open AccessSemi-active Control of Landing Gear with MR Damper
Author(s) -
Hüseyin BALTA,
Rahmi Güçlü
Publication year - 2016
Publication title -
uluslararası mühendislik araştırma ve geliştirme dergisi
Language(s) - English
Resource type - Journals
eISSN - 1308-5514
pISSN - 1308-5506
DOI - 10.29137/umagd.346135
Subject(s) - damper , suspension (topology) , vibration , voltage , work (physics) , vibration control , damping torque , structural engineering , control theory (sociology) , nonlinear system , engineering , computer science , physics , control (management) , acoustics , mechanical engineering , mathematics , electrical engineering , artificial intelligence , pure mathematics , induction motor , homotopy , direct torque control , quantum mechanics
In this work, an aircraft landing gear vibrations having passive suspension system, has been tried to reduce by a MR damper semiactive suspension system. MR damper being a semi-active component, has a nonlinear character and its damping force can be changed with the voltage applied to MR damper. For this purpose, the design of voltage sent to MR damper was done depending on the status of volt 2. The damping force is changed with the voltage determined and vibrations can be reduced with the help of MR dampers. The result of simulation works showed that the voltage applied to the MR damper has an active role in reducing vibration.
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