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
Link To Document :
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