SEMI ACTIVE CONTROL OF FIGHTER JET LANDING GEAR COMPARING WITH PID AND FUZZY LOGIC CONTROLLER EQUIPPED MAGNETORHEOLOGICAL DAMPER
Abstract
Keywords
References
- ⦁ Currey N.S., (1988) Aircraft Landing Gear Design: Principles and Practices. Washington D.C.: American Institute of Aeronautics and Astronautics, Inc..
- ⦁ Winslow W.M., (1949) Induced Fibration of Suspensions, Journal of Applied Physics, 20 (12):1137–1140.
- ⦁ Rabinow J., (1951) Magnetic Fluid Torque and Force Transmitting Device, U.S. Patent Number:2,575,360.
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- ⦁ Saxena D., Rathore H., (2013) Vibration Control of MR Damper Landing Gear, International Journal of Advanced Research in Artificial Intelligence, Vol. 2, No.3.
- ⦁ Margolis D.L., (1983) a Procedure for Comparing Passive, Active And Semi-Active Approaches to Vibration Isolation, Journal of the Franklin Institute, Vol. 315, pp. 225-238.
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Details
Primary Language
English
Subjects
-
Journal Section
Research Article
Authors
Ömer Faruk Sancak
This is me
0000-0001-7411-1553
Türkiye
Rahmi Güçlü
This is me
0000-0003-0996-7923
Türkiye
Publication Date
December 1, 2018
Submission Date
April 16, 2018
Acceptance Date
November 25, 2018
Published in Issue
Year 2018 Volume: 36 Number: 4