DYNAMIC MODELING AND CONTROL OF AN ELECTRO-MECHANICAL FIN LOADING SYSTEM

Yıl 2022, , 1163 - 1176, 31.12.2022

Bülent Özkan

https://doi.org/10.17482/uumfd.1121360

Öz

In this study, the design of an electro-mechanical fin loading system which is utilized to simulate the effects of the aerodynamic moment occurring in an atmospheric flight on a missile system is dealt with. In this extent, the dynamic modeling of the dedicated loading system is constructed and then the control system is designed on that model. As the control algorithm, the classical control system operating with regard of the PID (proportional plus integral plus derivative) control action and the robust control system designed according to the H∞ norm are taken into consideration. Once the mentioned control systems are built, the relevant computer simulations are performed with the inclusion of a realistic control actuation system model in accordance with the consistent numerical values of the necessary parameters. As a result of this work, it is observed that the robust control system yields more satisfactory results than its classical counterpart even under more severe conditions.

Anahtar Kelimeler

fin loading system, classical control, robust control, aerodynamic load, control actuation system

Elektromekanik Eyletimli Bir Kanat Yükleme Cihazının Dinamik Modellemesi ve Denetimi

Öz

Bu çalışmada, atmosfer içerisinde uçan bir füzeye etkiyen aerodinamik moment etkisinin yerde benzetimini yapmak amacıyla tasarlanan elektromekanik eyletimli bir kanat yükleme cihazının tasarımı ele alınmaktadır. Bu kapsamda, göz önüne alınan kanat yükleme cihazının dinamik modeli çıkarılmış ve ardından bu model üzerine denetim sistemi tasarlanmıştır. Denetim sistemi olarak, PID (oransal, tümlevsel ve türevsel) denetim işlemini esas alan klasik denetim sistemi ile H∞ normunu esas alarak sentezlenen gürbüz denetim sistemi uygulanmıştır. Denetim sistemi oluşturulduktan sonra, ilgili parametreler için belirlenen tutarlı sayısal değerler kullanılarak modellenen gerçekçi bir kontrol tahrik sistemi de toplam sistem şemasına dahil edilerek bilgisayar benzetimleri gerçekleştirilmiştir. Benzetimler sonucunda, çok daha zorlu işletim koşulları altında dahi gürbüz denetim sisteminin klasik denetim sistemine nazaran daha tatminkâr çıktılar ürettiği gözlenmiştir.

Anahtar Kelimeler

kanat yükleme cihazı, klasik denetim, gürbüz denetim, aerodinamik yük, kontrol tahrik sistemi

Kaynakça

• 1. Arulmozhiyal, R., Murali, M. and Manikanadan, R. (2015) Modeling and simulation of control actuation system, ARPN Journal of Engineering and Applied Sciences, 10 (4), 1778-1782.
• 2. Blasi, L., Borrelli, M., D’Amato, E., di Grazia, L. E., Mattei, M. and Notaro, I. (2021) Modeling and control of a modular iron bird, Aerospace, 8(2), 39. doi: 10.3390/aerospace8020039
• 3. Borrelli, M., D’Amato, E., Emanuel di Grazia, L., Mattei, M. and Notaro, I. (2020). MPC load control for aircraft actuator testing, 2020 7th International Conference on Control, Decision and Information Technologies (CoDIT), Prague, Czech Republic.
• 4. https://www.ideal-aerosmith.com/ideal-product/aeroload-simulation-system, Date of access: 25.05.2022, Subject: Aerodynamic Loading System.
• 5. Jing, C. H., Xu, H. G. and Jiang, J. H. (2019). Dynamic surface disturbance rejection control for electro-hydraulic load simulator, Mech. Syst. Signal. Process. 134.
• 6. Kassem, A. M., Sayed, K., El-Zohri, E. H. and Ali, H. H. (2017) An integral square error-based model predictive controller for two area load frequency control, Advances in Energy Research, 5(1), 79-90. doi: 10.12989/eri.2017.5.1.079
• 7. Low K. H., Wang, H. and Wang M. Y. (2005) On the development of a real time control system by using xPC target: Solution to robotic system control, 2005 IEEE International Conference on Automation Science and Engineering, Edmonton, Canada, 345-350.
• 8. Maekawa, H. (1999) Compact servo driver for torque control of DC-servo motor based on voltage control, 1999 IEEE/ASME International Conference on Advanced Intelligent Mechatronics, Atlanta, USA, 341-346.
• 9. Muniraj, M. and Arulmozhiyal, R. (2015) Modeling and simulation of control actuation system with fuzzy-PID logic conrolled brushless motor drives for missiles glider applications, The Scientific World Journal, Hindawi Publishing Corporation, 1-11. doi: 10.1155/2015/723298
• 10. Nam, Y., Lee, J. and Sung K. H. (2000) Force control system design for aerodynamic load simulator, American Control Conference, Chicago, Illinois, USA, 3043-3046.
• 11. Ogata K. (1997) Modern Control Engineering, Third Edition, Prentice-Hall, USA.
• 12. Özkan B. (2005) Dynamic Modeling, Guidance and Control of Homing Missiles, PhD Thesis, Mechanical Engineering Department, Middle East Technical University, Ankara, Turkey.
• 13. Özkan, B. (2017) Dynamic modeling and control of a hydraulic fin loading system using ıntegral backstepping method, Dokuz Eylül University, Faculty of Engineering Journal of Science and Engineering, 19-56. doi: 10.21205/deufmd.2017195636
• 14. Özkan B., Yıldız E. N. and Dönmez B. (2008) Precise position control of a gimbaled camera system, AIAA Guidance, Navigation, and Control Conference and Exhibit, Honolulu, Hawaii, USA.
• 15. Özakalın, M. U., Salamci, M. U. and Özkan, B. (2014) Implementation of the sliding mode control with constant and varying sliding surfaces to a hydraulically-actuated fin loading system, 19th IFAC World Congress, Cape Town, South Africa.
• 16. Page J. L. and Willis K. E. (1998) Designing motion systems for hardware-in-the-loop simulation, Carco Electronics Publications, USA.
• 17. Tekin, R. and Şahin, M. (2008) Development of a test device fort he loading tests of a missile control actuation system (in Turkish), SAVTEK 2008-Defense Technologies Conference, 601-607, Middle East Technical University, Ankara, Turkey.