Research Article

SEMI ACTIVE CONTROL OF FIGHTER JET LANDING GEAR COMPARING WITH PID AND FUZZY LOGIC CONTROLLER EQUIPPED MAGNETORHEOLOGICAL DAMPER

Volume: 36 Number: 4 December 1, 2018
  • Ömer Faruk Sancak
  • Rahmi Güçlü

SEMI ACTIVE CONTROL OF FIGHTER JET LANDING GEAR COMPARING WITH PID AND FUZZY LOGIC CONTROLLER EQUIPPED MAGNETORHEOLOGICAL DAMPER

Abstract

This paper associated with a fighter jet landing gears that has semi active suspension system. Aircraft landing gears are most important part of the aircraft during taxi position which must be able to reduce vibrations from runway roughness. For this purpose, Magnetorheological (MR) damper is used instead of passive damper as semi active landing gear and its damping force varies by voltage controller which is applied to electromagnetic coil. In order to determine the applied voltage, fuzyy logic controller and PID controller are designed. The performance of MR damper is shown with extensive numbers of numerical simulations. The two control methods are compared with each other. It is shown that the controllers can be applicable to the system and is shown that why the semi active systems can be more preferable.

Keywords

References

  1. ⦁ Currey N.S., (1988) Aircraft Landing Gear Design: Principles and Practices. Washington D.C.: American Institute of Aeronautics and Astronautics, Inc..
  2. ⦁ Winslow W.M., (1949) Induced Fibration of Suspensions, Journal of Applied Physics, 20 (12):1137–1140.
  3. ⦁ Rabinow J., (1951) Magnetic Fluid Torque and Force Transmitting Device, U.S. Patent Number:2,575,360.
  4. ⦁ Kordonsky W., (1993) Magnetorheological Effect As a Base of New Devices and Technologies, Journal of Magnetism and Magnetic Materials, 122:395-398.
  5. ⦁ Spencer B.F.Jr., Dyke S.J., Sain M.K., Carlson J.D., (1997) Phenomenological Model of a Magnetorheological Damper, Journal of Engineering Mechanics, ASCE, 123(3):230-238.
  6. ⦁ Saxena D., Rathore H., (2013) Vibration Control of MR Damper Landing Gear, International Journal of Advanced Research in Artificial Intelligence, Vol. 2, No.3.
  7. ⦁ 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.
  8. ⦁ Yuan I., Hac A., (1995) Semi-Active Suspensions with Adaptive Capability, Journal of Sound and Vibration, Vol. 180, pp.475-492.

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

APA
Sancak, Ö. F., & Güçlü, R. (2018). SEMI ACTIVE CONTROL OF FIGHTER JET LANDING GEAR COMPARING WITH PID AND FUZZY LOGIC CONTROLLER EQUIPPED MAGNETORHEOLOGICAL DAMPER. Sigma Journal of Engineering and Natural Sciences, 36(4), 1215-1234. https://izlik.org/JA89MS38YA
AMA
1.Sancak ÖF, Güçlü R. SEMI ACTIVE CONTROL OF FIGHTER JET LANDING GEAR COMPARING WITH PID AND FUZZY LOGIC CONTROLLER EQUIPPED MAGNETORHEOLOGICAL DAMPER. SIGMA. 2018;36(4):1215-1234. https://izlik.org/JA89MS38YA
Chicago
Sancak, Ömer Faruk, and Rahmi Güçlü. 2018. “SEMI ACTIVE CONTROL OF FIGHTER JET LANDING GEAR COMPARING WITH PID AND FUZZY LOGIC CONTROLLER EQUIPPED MAGNETORHEOLOGICAL DAMPER”. Sigma Journal of Engineering and Natural Sciences 36 (4): 1215-34. https://izlik.org/JA89MS38YA.
EndNote
Sancak ÖF, Güçlü R (December 1, 2018) SEMI ACTIVE CONTROL OF FIGHTER JET LANDING GEAR COMPARING WITH PID AND FUZZY LOGIC CONTROLLER EQUIPPED MAGNETORHEOLOGICAL DAMPER. Sigma Journal of Engineering and Natural Sciences 36 4 1215–1234.
IEEE
[1]Ö. F. Sancak and R. Güçlü, “SEMI ACTIVE CONTROL OF FIGHTER JET LANDING GEAR COMPARING WITH PID AND FUZZY LOGIC CONTROLLER EQUIPPED MAGNETORHEOLOGICAL DAMPER”, SIGMA, vol. 36, no. 4, pp. 1215–1234, Dec. 2018, [Online]. Available: https://izlik.org/JA89MS38YA
ISNAD
Sancak, Ömer Faruk - Güçlü, Rahmi. “SEMI ACTIVE CONTROL OF FIGHTER JET LANDING GEAR COMPARING WITH PID AND FUZZY LOGIC CONTROLLER EQUIPPED MAGNETORHEOLOGICAL DAMPER”. Sigma Journal of Engineering and Natural Sciences 36/4 (December 1, 2018): 1215-1234. https://izlik.org/JA89MS38YA.
JAMA
1.Sancak ÖF, Güçlü R. SEMI ACTIVE CONTROL OF FIGHTER JET LANDING GEAR COMPARING WITH PID AND FUZZY LOGIC CONTROLLER EQUIPPED MAGNETORHEOLOGICAL DAMPER. SIGMA. 2018;36:1215–1234.
MLA
Sancak, Ömer Faruk, and Rahmi Güçlü. “SEMI ACTIVE CONTROL OF FIGHTER JET LANDING GEAR COMPARING WITH PID AND FUZZY LOGIC CONTROLLER EQUIPPED MAGNETORHEOLOGICAL DAMPER”. Sigma Journal of Engineering and Natural Sciences, vol. 36, no. 4, Dec. 2018, pp. 1215-34, https://izlik.org/JA89MS38YA.
Vancouver
1.Ömer Faruk Sancak, Rahmi Güçlü. SEMI ACTIVE CONTROL OF FIGHTER JET LANDING GEAR COMPARING WITH PID AND FUZZY LOGIC CONTROLLER EQUIPPED MAGNETORHEOLOGICAL DAMPER. SIGMA [Internet]. 2018 Dec. 1;36(4):1215-34. Available from: https://izlik.org/JA89MS38YA

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