Active Control of Shimmy Vibration in Aircraft Nose Landing Gear using Fuzzy and NARMA-L2 Controllers

In this paper, control of shimmy vibration of aircraft nose landing gear is presented. In this regard, the NARMA-L2 neural controller and a robust controller using a fuzzy method are designed and compared. The efficiency of these controllers was measured by comparing the results obtained from CTM an...

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Bibliographic Details
Main Authors: Milad Yazdanpanah, Alireza Nateghi, hassan Zare
Format: Article
Language:English
Published: Islamic Azad University-Isfahan (Khorasgan) Branch 2023-06-01
Series:International Journal of Advanced Design and Manufacturing Technology
Subjects:
Online Access:https://admt.isfahan.iau.ir/article_702363_f6a2e62679277b4e9f76fe830eef3d45.pdf