Araştırma Makalesi
BibTex RIS Kaynak Göster

PWM Controlled Servomechanism

Yıl 2023, Cilt: 7 Sayı: 3, 324 - 329, 15.11.2023
https://doi.org/10.30518/jav.1351782

Öz

Precise control of aircraft flight control surfaces by the pilot is critical to flight safety. The joystick and control surface positions must be detected accurately and quickly, and the motion mechanism must be operated in such a way as to ensure synchronization between them. The analogue voltage value taken from the potentiometer, which is used as a position sensor in many small aircraft, can be used directly or by converting to digital.
In this applied study, the analogue position knowledge received from the potentiometer on the joystick was converted into a PWM signal with an oscillator circuit. The PWM position signal applied to the IR (InfraRed) LED in the transmitter unit is sent as infrared light. The PWM position knowledge detected by the photodiode in the receiver unit was passed through the LPF (Low Pass Filter) and the voltage value of the joystick potentiometer was obtained again. With the mechanism controlled according to the difference between the potentiometer values of the joystick and the control surface, the synchronization between the joystick and the control surface is ensured. In this study, a wireless and stable servomechanism connection is obtained by transmitting PWM position knowledge as IR.

Kaynakça

  • Bandyopadhyay, M., Mandal, N. and Chattopadhyay, S. (2016). Position Control System of A PMDC Motor. International Conference on Electrical, Electronics, and Optimization Techniques (ICEEOT). 752-754.
  • Çoban, S. and Oktay, T. (2023). Innovative Morphing UAV Design and Manufacture. Journal of Aviation. 7 (2), 184-189.
  • Çoban, S. and Oktay, T. (2018). Simultaneous Design of a Small UAV (Unmanned Aerial Vehicle) Flight Control System and Lateral State Space Model. Journal of Aviation. 2 (2), 70-76.
  • Çoban, S. and Oktay, T. (2018). Unmanned Aerial Vehicles (UAVs) According to Engine Type. Journal of Aviation. 2 (2), 177-184.
  • Düzgün, M. (2021). Investigation of the Criteria Affecting the Decision of Use of Drone Technology in the Logistics Sector by DEMATEL Method. Journal of Aviation. 5(2), 249-264.
  • Hu, M., Yu, E. and Yan, W. (2021). Design of Highly Deterministic and Reliable Aircraft Electronic-Mechanical Actuator Servo Control System. IEEE International Conference on Electrical Engineering and Mechatronics Technology (ICEEMT 2021). 459-463.
  • Kim, Y. and Choi, H.Y. (2018). Development of High-Temperature Position Sensors for Control of Actuators in Aerospace Systems. 9th International Conference on Mechanical and Aerospace Engineering. 6-10.
  • Kekeç, E.T., Konar, M. and Yıldırım Dalkıran, F. (2020). Realization of Low-Cost Useful Variometer Application for Sportive Aviation. Journal of Aviation. 4(1), 79-88.
  • Konar, M. and Bilgin, M. (2022). Investigation of Visual Disappearance by Intelligent Illumination of Exterior Surfaces of Unmanned Aerial Vehicles. Journal of Aviation. 6(1), 26-32.
  • Koç, E., Çalışkan, C.I., Coşkun, M. and Khan, H.M. (2020). Unmanned Aerial Vehicle Production with Additive Manufacturing. Journal of Aviation. 4(1), 22-30.
  • Erşen, M. and Konar, M. (2023). Obtaining Condition Monitoring Data for the Prognostics of the Flight Time of Unmanned Aerial Vehicles. Journal of Aviation. 7 (2), 209-214.
  • Lang, Y. and Li, Y., (2009). Concept Design and Dynamic Response Analysis of Electro-Hydraulic Compound Regulating Integrated Actuator. IEEE/ASME International Conference on Advanced Intelligent Mechatronics. 1389-1394.
  • Luccena, S. and Suzuki, E.Y. (2007). Electro-Hydraulic Actuator Tester for Fly-By-Wire Aircrafts. Instrumentation and Measurement Technology Conference. Poland. 1-3.
  • Nguyen, T.A. and Konishi, S. (2013). Position Feedback Control of Electrostatically Controlled Linear Actuator System. MHS2013. 1-5.
  • Toman, J., Singule, V. and Hadas, Z. (2014). Model of Aircraft Actuator with BLAC Motor. 16th International Power Electronics and Motion Control Conference and Exposition. Türkiye. 197-202.
  • Wikipedia. Encyclopedia. Servomechanism. (2023, March 20). https://en.wikipedia.org/wiki/Servomechanism
  • Yıldırım Dalkıran, F. Gençağ, M.S. (2021). Increasing the Stabilization of Unmanned Aerial Vehicle in Global Navigation Satellite System Unavailable Areas. Journal of Aviation. 5(1), 36-44.
  • Zhou, S. and Wang, L. (2018). Research on Modeling and Simulation of aircraft cabin pressure regulating system based on stepper motor servo system. 21st International Conference on Electrical Machines and Systems (ICEMS). Korea. 938-942.
Yıl 2023, Cilt: 7 Sayı: 3, 324 - 329, 15.11.2023
https://doi.org/10.30518/jav.1351782

Öz

Kaynakça

  • Bandyopadhyay, M., Mandal, N. and Chattopadhyay, S. (2016). Position Control System of A PMDC Motor. International Conference on Electrical, Electronics, and Optimization Techniques (ICEEOT). 752-754.
  • Çoban, S. and Oktay, T. (2023). Innovative Morphing UAV Design and Manufacture. Journal of Aviation. 7 (2), 184-189.
  • Çoban, S. and Oktay, T. (2018). Simultaneous Design of a Small UAV (Unmanned Aerial Vehicle) Flight Control System and Lateral State Space Model. Journal of Aviation. 2 (2), 70-76.
  • Çoban, S. and Oktay, T. (2018). Unmanned Aerial Vehicles (UAVs) According to Engine Type. Journal of Aviation. 2 (2), 177-184.
  • Düzgün, M. (2021). Investigation of the Criteria Affecting the Decision of Use of Drone Technology in the Logistics Sector by DEMATEL Method. Journal of Aviation. 5(2), 249-264.
  • Hu, M., Yu, E. and Yan, W. (2021). Design of Highly Deterministic and Reliable Aircraft Electronic-Mechanical Actuator Servo Control System. IEEE International Conference on Electrical Engineering and Mechatronics Technology (ICEEMT 2021). 459-463.
  • Kim, Y. and Choi, H.Y. (2018). Development of High-Temperature Position Sensors for Control of Actuators in Aerospace Systems. 9th International Conference on Mechanical and Aerospace Engineering. 6-10.
  • Kekeç, E.T., Konar, M. and Yıldırım Dalkıran, F. (2020). Realization of Low-Cost Useful Variometer Application for Sportive Aviation. Journal of Aviation. 4(1), 79-88.
  • Konar, M. and Bilgin, M. (2022). Investigation of Visual Disappearance by Intelligent Illumination of Exterior Surfaces of Unmanned Aerial Vehicles. Journal of Aviation. 6(1), 26-32.
  • Koç, E., Çalışkan, C.I., Coşkun, M. and Khan, H.M. (2020). Unmanned Aerial Vehicle Production with Additive Manufacturing. Journal of Aviation. 4(1), 22-30.
  • Erşen, M. and Konar, M. (2023). Obtaining Condition Monitoring Data for the Prognostics of the Flight Time of Unmanned Aerial Vehicles. Journal of Aviation. 7 (2), 209-214.
  • Lang, Y. and Li, Y., (2009). Concept Design and Dynamic Response Analysis of Electro-Hydraulic Compound Regulating Integrated Actuator. IEEE/ASME International Conference on Advanced Intelligent Mechatronics. 1389-1394.
  • Luccena, S. and Suzuki, E.Y. (2007). Electro-Hydraulic Actuator Tester for Fly-By-Wire Aircrafts. Instrumentation and Measurement Technology Conference. Poland. 1-3.
  • Nguyen, T.A. and Konishi, S. (2013). Position Feedback Control of Electrostatically Controlled Linear Actuator System. MHS2013. 1-5.
  • Toman, J., Singule, V. and Hadas, Z. (2014). Model of Aircraft Actuator with BLAC Motor. 16th International Power Electronics and Motion Control Conference and Exposition. Türkiye. 197-202.
  • Wikipedia. Encyclopedia. Servomechanism. (2023, March 20). https://en.wikipedia.org/wiki/Servomechanism
  • Yıldırım Dalkıran, F. Gençağ, M.S. (2021). Increasing the Stabilization of Unmanned Aerial Vehicle in Global Navigation Satellite System Unavailable Areas. Journal of Aviation. 5(1), 36-44.
  • Zhou, S. and Wang, L. (2018). Research on Modeling and Simulation of aircraft cabin pressure regulating system based on stepper motor servo system. 21st International Conference on Electrical Machines and Systems (ICEMS). Korea. 938-942.
Toplam 18 adet kaynakça vardır.

Ayrıntılar

Birincil Dil İngilizce
Konular Uzay Mühendisliği (Diğer)
Bölüm Araştırma Makaleleri
Yazarlar

Mehmet Ali Soytürk 0000-0002-0923-5709

Yayımlanma Tarihi 15 Kasım 2023
Gönderilme Tarihi 29 Ağustos 2023
Kabul Tarihi 4 Ekim 2023
Yayımlandığı Sayı Yıl 2023 Cilt: 7 Sayı: 3

Kaynak Göster

APA Soytürk, M. A. (2023). PWM Controlled Servomechanism. Journal of Aviation, 7(3), 324-329. https://doi.org/10.30518/jav.1351782

Journal of Aviation - JAV 


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