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

Yıl 2018, Cilt: 36 Sayı: 4, 1215 - 1234, 01.12.2018

Ömer Faruk Sancak Rahmi Güçlü

Öz

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.

Anahtar Kelimeler

Aircraft landing gear, seated pilot model, MR damper, taxiing analysis, semi active control, fuzzy logic control, PID control, particle swarm optimization.

Kaynakça

• ⦁ 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.
• ⦁ Kordonsky W., (1993) Magnetorheological Effect As a Base of New Devices and Technologies, Journal of Magnetism and Magnetic Materials, 122:395-398.
• ⦁ 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.
• ⦁ 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.
• ⦁ Yuan I., Hac A., (1995) Semi-Active Suspensions with Adaptive Capability, Journal of Sound and Vibration, Vol. 180, pp.475-492.
• ⦁ Sims N.D., Stanway R., (2003) Semi-Active Vehicle Suspensions Using Smart Fluids Dampers: a Modeling and Control Study, International Journal of Vehicle Design, Vol. 33, pp.76-102.
• ⦁ Kruger W., (2002) Design and Simulation of Semi-Active Landing Gears for Transport Aircraft, Mechanics of Structures and Mechanics, Vol. 30, pp. 493-526.
• ⦁ Hua-Lin L. et al., (2009) Fuzzy PID Control for Landing Gear Based on Magneto-rheological (MR) Damper, International Conference on Apperceiving Computing and Intelligence Analysis, pp. 22-25, Chengdu.
• ⦁ Choi Y.T., Wereley N.M., (2003) Vibration Control of a Landing Gear System Featuring ER/MR Fluids, Journal of Aircraft, Vol. 40, pp. 432-439.
• ⦁ Sivakumar S., Haran A. P., (2012) Parametric Analysis and Vibration Control of Landing Gear with PID Controller, European Journal of Scientific Research, vol. 89, pp. 441-453.
• ⦁ Sateesh, B., Maiti, D. K., (2010) Vibration Control of an Aircraft Nose Landing Gear Due to Ground-Induced Excitation, Proceedings of the Institution of Mechanical Engineers, Part G:, Vol. 224, No. 3, 245–258.
• ⦁ Sancak, O.F., Paksoy, M., Cetin, S., (2016) Vibration Reduction of an Aircraft Using Semi Active Landing Gear with MR Damper, Conference on Advances in Mechanical Engineering, 506-511, 11-13 May, Istanbul.
• ⦁ Gharapurkar A.A.,(2014) Robust Semi-Active Control of Aircraft Landing Gear System Equipped with Magnetorheological Dampers, Master Thesis, Concordia University, Montreal, Quebec Canada.
• ⦁ Paksoy M., Guclu R. (2013) Taşıt Titreşimlerinin MR Sönümleyici ile Yarı Aktif Bulanık Kontrolü, MSc Thesis, Graduate School of Natural and Applied Sciences, YTU, Istanbul Turkey.
• ⦁ Yildiz A.S., Sivrioglu S., (2013) Çeyrek Taşıt Sisteminin MR Sönümleyici ile Uyarlamalı Yarı Aktif Kontrolü, MSc Thesis, Graduate School of Natural and Applied Sciences, GYTE, Kocaeli Turkey.
• ⦁ Sever M., Yazici H., (2016) Observed Based Optimal Vibration Control of a Full Aircraft System Having Active Landing Gear and Biodynamic Pilot Model, Shock and Vibration, Vol. 2016, DOI:10.1155/2016/2150493.
• ⦁ Talib M.H.A., Darus I.Z.M., (2014) Development of Fuzzy Logic Controller by Particle Swarm Optimization Algorithm for Semi-Active Suspension System Using Magneto-rheological Damper, WSEAS Transactions on Systems and Contol, Vol 9, E-ISSN: 2224-2856.