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Yazdanpanah, Milad, Nateghi, Alireza, Zare, hassan. (1402). Active Control of Shimmy Vibration in Aircraft Nose Landing Gear using Fuzzy and NARMA-L2 Controllers. نشریه علمی پژوهشی دانشگاه آزاد اسلامی, 16(2), 55-64. doi: 10.30486/admt.2023.1965079.1373
Milad Yazdanpanah; Alireza Nateghi; hassan Zare. "Active Control of Shimmy Vibration in Aircraft Nose Landing Gear using Fuzzy and NARMA-L2 Controllers". نشریه علمی پژوهشی دانشگاه آزاد اسلامی, 16, 2, 1402, 55-64. doi: 10.30486/admt.2023.1965079.1373
Yazdanpanah, Milad, Nateghi, Alireza, Zare, hassan. (1402). 'Active Control of Shimmy Vibration in Aircraft Nose Landing Gear using Fuzzy and NARMA-L2 Controllers', نشریه علمی پژوهشی دانشگاه آزاد اسلامی, 16(2), pp. 55-64. doi: 10.30486/admt.2023.1965079.1373
Yazdanpanah, Milad, Nateghi, Alireza, Zare, hassan. Active Control of Shimmy Vibration in Aircraft Nose Landing Gear using Fuzzy and NARMA-L2 Controllers. نشریه علمی پژوهشی دانشگاه آزاد اسلامی, 1402; 16(2): 55-64. doi: 10.30486/admt.2023.1965079.1373

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

ADMT Journal
دوره 16، شماره 2، شهریور 2023، صفحه 55-64    اصل مقاله (717.32 K)
نوع مقاله: Original Article
شناسه دیجیتال (DOI): 10.30486/admt.2023.1965079.1373
نویسندگان
Milad Yazdanpanah1؛ Alireza Nateghi2؛ hassan Zare* 3
1Department of Electrical Engineering, science and research branch of Azad University, Iran
2Faculty of Electrical and Computer Engineering, Shahid Sattari University of Aeronautical Engineering, Iran
3Department of Electrical Engineering, Technical and Vocational University (TVU), Iran
چکیده
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 and PID controllers. Using the NARMA-L2 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.
کلیدواژه‌ها
Aircraft؛ Fuzzy Controller؛ NARMA-L2؛ Neural Controller؛ Suspension Oscillations
مراجع
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