Title of article
Active Control of Shimmy Vibration in Aircraft Nose Landing Gear using Fuzzy and NARMA-L2 Controllers
Author/Authors
Yazdanpanah ، Milad Department of Electrical Engineering - science and research branch of Azad University , Nateghi ، Alireza Faculty of Electrical and Computer Engineering - Shahid Sattari University of Aeronautical Engineering , Zare ، hassan Department of Electrical Engineering - Technical and Vocational University (TVU)
From page
55
To page
64
Abstract
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.
Keywords
Aircraft , Fuzzy controller , NARMA , L2 , Neural Controller , Suspension Oscillations
Journal title
International Journal of Advanced Design and Manufacturing Technology
Journal title
International Journal of Advanced Design and Manufacturing Technology
Record number
2743743
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