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State Feedback H∞ Semi Active Control of Fighter Jet Seat

Yıl 2019, Cilt: 60 Sayı: 694, 32 - 49, 19.03.2019

Öz

This paper deals with the design of a Linear Matrix Inequalities (LMI) based state feedback H∞ controller for a semi active vibration mitigation problem of fighter jet seats. Ten degrees of freedom detailed full aircraft mathematical model having semi active seats are controlled and analyzed seat vibrations caused by runway excitations during taxiing. For this purpose a Magneto-Rheological (MR) damper is used instead of a passive damper as semi active seats. The MR damper has non-linear characteristics and its damping force varies by voltage which is applied to electromagnetic coil. The performance of seats with the MR damper is controled via LMI based state feedback H∞ controller. The control method is compared with the passive case (MR 0 V).   

Kaynakça

  • 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.
  • Ahan, A. O., Arisoy, D. O., Muderrisoglu, K., Yazici, H., Guclu, R. 2016. “Vibration Control of A Semi-Trailer Truck for Comfort with an Output Feedback Controller,” International Conference on Engineering and Natural Science, 24-28 May, Sarajevo.
  • Guclu, R. 2004. “The Fuzzy-Logic Control of Active Suspensions without Suspension-Gap Degeneration,” Journal of Mechanical Engineering-Strojniski Vestnik, vol. 50(10), p. 462-468.
  • Guclu, R., Gulez, K. 2008. “Neural Network Control of Seat Vibrations of a Non-linear Full Vehicle Model using PMSM,” Mathematical and Computer Modelling, DOI: 10.1016/j.mcm.2007.08.013, vol. 47(11-12), p. 1356-1371.
  • Paksoy, M., Guclu, R., Cetin, S. 2014. “Semiactive Self-Tuning Fuzzy Logic Control of Full Vehicle Model with MR Damper,” Advances in Mechanical Engineering, DOI:10.1155/2014/816813, vol. 2014, Article ID 816813.
  • Wang, H. 2008. “An Investigation of an Active Landing Gear System to Reduce Aircraft Vibrations Caused by Landing Impacts and Runway Excitations,” Journal of Sound and Vibration, vol. 317, 50-66. 133.
  • Sivakumar, S., Haran, A. P. 2012. “Parametric Analysis and Vibration Control of Landing Gear with PID Controller,” European Journal of Scientific Research, vol. 89, p. 441-453.
  • Zapateiro, M. 2011. “Landing Gear Suspension Control Through Adaptive Backstepping Techniques with H∞ Performance,” Proc. The 18th IFAC World Congress., p. 4809-4814, Milano.
  • Margolis, D. L. 1983. “A Procedure for Comparing Passive, Active and Semi-Active Approaches to Vibration Isolation”, Journal of the Franklin Institute, vol. 315, p. 225-238.
  • Youn, I., Hac, A. 1995. “Semi-Active Suspensions with Adaptive Capability,” Journal of Sound and Vibration, vol. 180, p. 475-492.
  • Sims, N.D., Stanway, R. 2003. “Semi-Active Vehicle Suspension Using Smart Fluid Dampers: a Modeling and Control Study”, International Journal of Vehicle Design, vol. 33, 76-102.
  • Mikulowski, G., Holnicki-szulc, J. 2003. “Adaptive Aircraft Shock Absorbers”, AMAS Workshop on Smart Materials and Structures, vol. 3, p. 63-72.
  • Kruger, W. 2002. “Design and Simulation of Semi-Active Landing Gears for Transport Aircraft”, Mechanics of Structures and Machines, vol. 30, p. 493-526.
  • Choi, Y. T., Wereley, N. M. 2003. “Vibration Control of a Landing Gear System Featuring ER/MR Fluids”, Journal of Aircraft, vol. 40, p. 432-439.
  • Ghiringhelli, G. L. 2000. “Testing of a Semi-Active Landing Gear Control for a General Aviation Aircraft”, Journal of Aircraft, vol. 37, p. 606-616.
  • Wang, E. R. 2003. “Semi-Active Control of Vehicle Vibration with MR-Dampers”, Proc. 42nd IEEE Conference on Decision and Control, vol. 3, 2270-2275.
  • Kim, K., Jeon, D. 1999. “Vibration Suppression in an MR Fluid Damper Suspension System”, Journal of Intelligent Material Systems and Structures, vol. 10, p. 779-786.
  • Lam, H.F., Liao, W. S. 2003. “Semi-Active Control of Automobile Suspension Systems with Magnetorheological Dampers”, International Journal of Vehicle Design, vol. 33, 1-3.
  • Gharapurkar, A. A. 2014. “Robust Semi-Active Control of Aircraft Landing Gear System Equipped with Magnetorheological Dampers,” Master Thesis, Concordia University, Montreal, Canada.
  • Paksoy, M., Guclu, R. 2013. “Taşıt Titreşimlerinin MR Sönümleyici ile Yarı Aktif Bulanık Kontrolü,” Yüksek Lisans Tezi, YTÜ, Fen Bilimleri Enstitüsü, İstanbul, Türkiye.
  • Yıldız, A. S., Sivrioğlu, S. 2013. “Çeyrek Taşıt Sisteminin MR Sönümleyici ile Uyarlamalı Yarı Aktif Kontrolü,” Yüksek Lisans Tezi, GYTE, Fen Bilimleri Enstitüsü, Kocaeli.
  • Francis, B. A. 1987. “A Course in H∞ Control Theory,” Lecture Notes in Control and Information Sciences 88, Edited by M.Thoma and A. Wyner, Springer-Verlag.
  • Doyle, J. C., Glover, K., Khargonekar, P. P., Francis, B. A. 1996. “State-Space Solutions to Standart H2 and 𝐻∞ Control Problems,” IEEE Transactions on Automatic Control, 34(8), p. 831–847.
  • Azeloğlu, C. O., Sağırlı, A. 2012. “LMI Based Mixed H2/H∞ State-Feedback Control of Crane Structures Against Earthquake Induced Vibration,” Journal of Engineering and Natural Sciences, Sigma30, p. 281-291.
  • Yazici, H., Guclu, R. 2011. “Active Vibration Control of Seismic Excited Structural System Using LMI-Based Mixed State Feedback Controller,” Turk J. Elec. Eng & Comp. Sci., vol.19, no. 6, DOI:10.3906/elk-1007-592. 2011.
  • Yazıcı, H., Küçükdemiral, İ. Beklan, Karadeniz, O. 2013. “Doyumlu Eyleyiciye Sahip Durum-Geri Beslemeli H∞ Kontrolör ile Otonom Bir Helikopterin Askıda Kalma Kontrolü,” TOK 2013, 26-28 Eylül 2013, Malatya.
  • Boyd, S., Ghaoui, L.E., Feron, E., Balakrishnan, V. 1994. “Linear Matrix Inequalities in System and Control Theory,” Society for Industrial and Applied Mathemetics, Philadelphia.
  • Löfberg, J. 2004. “Yalmip: A Toolbox for Modeling and Optimization in MATLAB,” Proceedings of the CACSD Conference, Taipei, Taiwan.
  • Strum, J. F., 1999. “Using SeDuMi 1.02 a Matlab for Optimization over Symmetric Cones”, Optimization Methods and Software, 11(2):625-653.

Savaş Uçağı Koltuğunun Durum Geri Beslemeli H∞ Yarı Aktif Kontrolü

Yıl 2019, Cilt: 60 Sayı: 694, 32 - 49, 19.03.2019

Öz

Bu çalışmada savaş uçağı koltuklarının yarı aktif titreşim azaltma problemi için Doğrusal Matris Eşitsizlikleri (DME) tabanlı durum geri beslemeli H∞ kontrolcü tasarlanması gerçekleştirilmiştir. Uçağın pistteki taksi hareketi esnasında yoldan gelen uyarıların sebep olduğu, on serbestlik dereceli yarı aktif koltuklara sahip tam uçağın matematiksel modelinin koltuk titreşimlerinin kontrolü ve analizi yapılmıştır. Bu amaçla, yarı aktif koltuklar olarak pasif sönümleyici yerine Manyeto-Reolojik (MR) sönümleyici kullanılmıştır. MR sönümleyici doğrusal olmayan karaktere sahiptir ve sönümleme kuvveti elektromanyetik sargılara uygulanan gerilim ile değişir. MR sönümleyicili koltukların performansı DME tabanlı durum geri beslemeli H∞ kontrolcü ile sağlanmıştır. Kontrol yöntemi sistemin pasif hali (MR 0 V) ile karşılaştırılmıştır.

Kaynakça

  • 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.
  • Ahan, A. O., Arisoy, D. O., Muderrisoglu, K., Yazici, H., Guclu, R. 2016. “Vibration Control of A Semi-Trailer Truck for Comfort with an Output Feedback Controller,” International Conference on Engineering and Natural Science, 24-28 May, Sarajevo.
  • Guclu, R. 2004. “The Fuzzy-Logic Control of Active Suspensions without Suspension-Gap Degeneration,” Journal of Mechanical Engineering-Strojniski Vestnik, vol. 50(10), p. 462-468.
  • Guclu, R., Gulez, K. 2008. “Neural Network Control of Seat Vibrations of a Non-linear Full Vehicle Model using PMSM,” Mathematical and Computer Modelling, DOI: 10.1016/j.mcm.2007.08.013, vol. 47(11-12), p. 1356-1371.
  • Paksoy, M., Guclu, R., Cetin, S. 2014. “Semiactive Self-Tuning Fuzzy Logic Control of Full Vehicle Model with MR Damper,” Advances in Mechanical Engineering, DOI:10.1155/2014/816813, vol. 2014, Article ID 816813.
  • Wang, H. 2008. “An Investigation of an Active Landing Gear System to Reduce Aircraft Vibrations Caused by Landing Impacts and Runway Excitations,” Journal of Sound and Vibration, vol. 317, 50-66. 133.
  • Sivakumar, S., Haran, A. P. 2012. “Parametric Analysis and Vibration Control of Landing Gear with PID Controller,” European Journal of Scientific Research, vol. 89, p. 441-453.
  • Zapateiro, M. 2011. “Landing Gear Suspension Control Through Adaptive Backstepping Techniques with H∞ Performance,” Proc. The 18th IFAC World Congress., p. 4809-4814, Milano.
  • Margolis, D. L. 1983. “A Procedure for Comparing Passive, Active and Semi-Active Approaches to Vibration Isolation”, Journal of the Franklin Institute, vol. 315, p. 225-238.
  • Youn, I., Hac, A. 1995. “Semi-Active Suspensions with Adaptive Capability,” Journal of Sound and Vibration, vol. 180, p. 475-492.
  • Sims, N.D., Stanway, R. 2003. “Semi-Active Vehicle Suspension Using Smart Fluid Dampers: a Modeling and Control Study”, International Journal of Vehicle Design, vol. 33, 76-102.
  • Mikulowski, G., Holnicki-szulc, J. 2003. “Adaptive Aircraft Shock Absorbers”, AMAS Workshop on Smart Materials and Structures, vol. 3, p. 63-72.
  • Kruger, W. 2002. “Design and Simulation of Semi-Active Landing Gears for Transport Aircraft”, Mechanics of Structures and Machines, vol. 30, p. 493-526.
  • Choi, Y. T., Wereley, N. M. 2003. “Vibration Control of a Landing Gear System Featuring ER/MR Fluids”, Journal of Aircraft, vol. 40, p. 432-439.
  • Ghiringhelli, G. L. 2000. “Testing of a Semi-Active Landing Gear Control for a General Aviation Aircraft”, Journal of Aircraft, vol. 37, p. 606-616.
  • Wang, E. R. 2003. “Semi-Active Control of Vehicle Vibration with MR-Dampers”, Proc. 42nd IEEE Conference on Decision and Control, vol. 3, 2270-2275.
  • Kim, K., Jeon, D. 1999. “Vibration Suppression in an MR Fluid Damper Suspension System”, Journal of Intelligent Material Systems and Structures, vol. 10, p. 779-786.
  • Lam, H.F., Liao, W. S. 2003. “Semi-Active Control of Automobile Suspension Systems with Magnetorheological Dampers”, International Journal of Vehicle Design, vol. 33, 1-3.
  • Gharapurkar, A. A. 2014. “Robust Semi-Active Control of Aircraft Landing Gear System Equipped with Magnetorheological Dampers,” Master Thesis, Concordia University, Montreal, Canada.
  • Paksoy, M., Guclu, R. 2013. “Taşıt Titreşimlerinin MR Sönümleyici ile Yarı Aktif Bulanık Kontrolü,” Yüksek Lisans Tezi, YTÜ, Fen Bilimleri Enstitüsü, İstanbul, Türkiye.
  • Yıldız, A. S., Sivrioğlu, S. 2013. “Çeyrek Taşıt Sisteminin MR Sönümleyici ile Uyarlamalı Yarı Aktif Kontrolü,” Yüksek Lisans Tezi, GYTE, Fen Bilimleri Enstitüsü, Kocaeli.
  • Francis, B. A. 1987. “A Course in H∞ Control Theory,” Lecture Notes in Control and Information Sciences 88, Edited by M.Thoma and A. Wyner, Springer-Verlag.
  • Doyle, J. C., Glover, K., Khargonekar, P. P., Francis, B. A. 1996. “State-Space Solutions to Standart H2 and 𝐻∞ Control Problems,” IEEE Transactions on Automatic Control, 34(8), p. 831–847.
  • Azeloğlu, C. O., Sağırlı, A. 2012. “LMI Based Mixed H2/H∞ State-Feedback Control of Crane Structures Against Earthquake Induced Vibration,” Journal of Engineering and Natural Sciences, Sigma30, p. 281-291.
  • Yazici, H., Guclu, R. 2011. “Active Vibration Control of Seismic Excited Structural System Using LMI-Based Mixed State Feedback Controller,” Turk J. Elec. Eng & Comp. Sci., vol.19, no. 6, DOI:10.3906/elk-1007-592. 2011.
  • Yazıcı, H., Küçükdemiral, İ. Beklan, Karadeniz, O. 2013. “Doyumlu Eyleyiciye Sahip Durum-Geri Beslemeli H∞ Kontrolör ile Otonom Bir Helikopterin Askıda Kalma Kontrolü,” TOK 2013, 26-28 Eylül 2013, Malatya.
  • Boyd, S., Ghaoui, L.E., Feron, E., Balakrishnan, V. 1994. “Linear Matrix Inequalities in System and Control Theory,” Society for Industrial and Applied Mathemetics, Philadelphia.
  • Löfberg, J. 2004. “Yalmip: A Toolbox for Modeling and Optimization in MATLAB,” Proceedings of the CACSD Conference, Taipei, Taiwan.
  • Strum, J. F., 1999. “Using SeDuMi 1.02 a Matlab for Optimization over Symmetric Cones”, Optimization Methods and Software, 11(2):625-653.
Toplam 32 adet kaynakça vardır.

Ayrıntılar

Birincil Dil Türkçe
Bölüm icindekiler-sunuş
Yazarlar

Rahmi Güçlü

Ömer Faruk Sancak

Yayımlanma Tarihi 19 Mart 2019
Gönderilme Tarihi 22 Nisan 2018
Kabul Tarihi 30 Temmuz 2018
Yayımlandığı Sayı Yıl 2019 Cilt: 60 Sayı: 694

Kaynak Göster

APA Güçlü, R., & Sancak, Ö. F. (2019). Savaş Uçağı Koltuğunun Durum Geri Beslemeli H∞ Yarı Aktif Kontrolü. Mühendis Ve Makina, 60(694), 32-49.

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ISSN : 1300-3402

E-ISSN : 2667-7520