Active Control of Shimmy Vibration in Aircraft Nose Landing Gear using Fuzzy and NARMA-L2 Controllers
الموضوعات :
Milad Yazdanpanah
1
,
Alireza Nateghi
2
,
hassan Zare
3
1 - Department of Electrical Engineering,
science and research branch of Azad University, Iran
2 - Faculty of Electrical and Computer Engineering,
Shahid Sattari University of Aeronautical Engineering, Iran
3 - Department of Electrical Engineering,
Technical and Vocational University (TVU), Iran
تاريخ الإرسال : 16 الأحد , محرم, 1444
تاريخ التأكيد : 25 الأربعاء , جمادى الثانية, 1444
تاريخ الإصدار : 12 الخميس , ذو القعدة, 1444
الکلمات المفتاحية:
Aircraft,
NARMA-L2,
Suspension Oscillations,
Neural Controller,
Fuzzy controller,
ملخص المقالة :
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.
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