Active Control of Shimmy Vibration in Aircraft Nose Landing Gear using Fuzzy and NARMA-L۲ Controllers
Publish place: International Journal of Advanced Design and Manufacturing Technology، Vol: 16، Issue: 2
Publish Year: 1402
نوع سند: مقاله ژورنالی
زبان: English
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شناسه ملی سند علمی:
JR_ADMTL-16-2_006
تاریخ نمایه سازی: 12 تیر 1402
Abstract:
In this paper, control of shimmy vibration of aircraft nose landing gear is presented. In this regard, the NARMA-L۲ 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 and PID controllers. Using the NARMA-L۲ neural controller, maximum effort and settling time are improved whereas using fuzzy controller overshoot of the vibration response improvement in the closed-loop system was observed. According to these results, a large part of the design requirements can be solved by the implemented controllers.
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Authors
Milad Yazdanpanah
Department of Electrical Engineering, science and research branch of Azad University, Iran
Alireza Nateghi
Faculty of Electrical and Computer Engineering, Shahid Sattari University of Aeronautical Engineering, Iran
hassan Zare
Department of Electrical Engineering, Technical and Vocational University (TVU), Iran
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