A mechatronic system for studying control processes on the example of a "Glide" type aircraft model

Authors

DOI:

https://doi.org/10.15588/1607-6761-2024-2-5

Keywords:

mechatronic system, aircraft, glider, control system, laboratory stand, modeling, Arduino, C

Abstract

Purpose. Development of a mechatronic system based on the example of a Glider type aircraft model for studying and researching its control processes.

Methodology. Physical experiment on the developed laboratory bench, computer modelling, calculation and analytical methods.

Findings. In the course of the study, the main processes of glider control were considered and analyzed: the interaction of the pilot's controls and the operating mechanisms of the wing. An analysis of the shortcomings and advantages of existing developments on the subject under study was carried out, taking into account the issues of mobility, economy, simplicity and reliability of implementation, as well as the possibility of using it as a training stand. A laboratory stand has been developed in the form of a mechatronic system based on the example of a "Glider" type aircraft model for studying and researching the interaction processes of control bodies and flight executive mechanisms. The software and hardware complex is connected using the USB interface. A SOC platform with an ArduinoUno microcontroller was used to process processor commands and convert them into aileron movements. The Logitech Extreme 3D joystick was chosen as the control interface. In order to increase the similarity to real systems, a certain delay (inertia) is provided between the moment of the operator's impact on the joystick and the response of the glider. Styrofoam was used as the material of the glider model. Servo drives MG-90S and DS-37 are used to control the position of the moving parts of the glider model. The airframe is rotated using a 28BYJ-48 engine. Software has been developed, the feature of which is easy setup and quick start-up of the laboratory stand. Provide for the possibility of keeping a log, which will allow analysis of the actions of the stand operator. As a result of the conducted research, the features of glider control and the structure of the mechanisms that ensure the control process were determined.

Originality. A mechatronic system of a "Glider" type aircraft model based on an ArduinoUno-based software-hardware complex has been proposed and developed, which differs from the existing ones by the presence of a program that provides easy setup and quick start-up of the aircraft, which allows you to study the interaction of control bodies and executive mechanisms flight.

Practical value. The developed laboratory stand based on the "Glider" type aircraft expands the possibilities of studying and researching electromechanical processes of automatic control systems of complex mechatronic objects.

Author Biographies

O.S. Nazarova, Zaporizhzhia Polytechnic National University

Candidate of Technical Science, associate professor, associate professor of the Electric Drive and Commercial Plant Automation Department, National University “Zaporizhzhia Polytechnic”

E.M. Kulynych, National University “Zaporizhzhia Polytechnic”

Candidate of Technical Science, associate professor, associate professor of the Electric Drive and Commercial Plant Automation Department, National University “Zaporizhzhia Polytechnic”

O.Yu. Berezhnyi, National University "Zaporizhzhia Polytechnic"

Student of the group Е-312-2 of the Electric Drive and Commercial Plant Automation Department, National University “Zaporizhzhia Polytechnic”

References

ICAO. Airplane upset prevention and recovery training aid [Electronic resource]. – Access mode: https://www.icao.int/safety/loci/AUPRTATablet/index.html.

Nazarova, O., Osadchyy, V., Hutsol, T., Glowacki, Sz., Nurek, T., Hulevskyi, V., Horetska I. (2024). Mechatronic automatic control system of electropneumatic manipulator. Scientific Reports, 14, 6970. https://doi.org/10.1038/s41598-024-56672-4.

Nae, C., Nicolin, I., Adrian, B. (2022). Nicolin Military Aircraft Flight Control. Aeronautics - New Advances. doi: 10.5772/intechopen.105491.

IVAO. Introduction to flight controls [Electronic resource]. – Access mode: https://wiki.ivao.aero/en/home/training/documentation/ Introduction_to_flight_controls.

U.S. Department of Transportation. Aviation Instruc-tor’s Handbook. [Electronic resource]. – Access mode: https://www.faa.gov/sites/faa.gov/files/regulations_policies/handbooks_manuals/aviation/aviation_instructors_handbook/aviation_instructors_handbook.pdf.

Kern, D. (2021). Introduction to Fly-by-Wire Flight Control Systems: The professional pilot’s guide to understanding aircraft controls. Paperback, 52.

Dupeyroux, J., Boutin, V., Serres, J. R., Perrinet, L. U. & S. (2018). Viollet M2APix: A Bio-Inspired Auto-Adaptive Visual Sensor for Robust Ground Height Estimation. 2018 IEEE International Symposium on Circuits and Systems (ISCAS), 1-4. doi: 10.1109/ISCAS.2018.8351433.

Żokowski, M. (2020). Autodiagnositcs for Remotely Piloted Aircraft Systems. International Conference Mechatronic Systems and Materials (MSM), 1-4. doi: 10.1109/MSM49833.2020.9201641.

Wang, M., Gu, W., Sun, Z., Zhang, Q., Li, J. (2020). Integrated Design and Verification Method of Air-craft and Propulsion System. 2020 IEEE Interna-tional Conference on Mechatronics and Automation (ICMA), Beijing, China, 1343-1347. doi: 10.1109/ICMA49215.2020.9233787.

Liu, T., Zhang, Y., Qian, Y., Ju, J., Yu, W. (2020). Sys-tem modeling and simulation for flap system power drive unit of commercial aircraft. CSAA/IET Interna-tional Conference on Aircraft Utility Systems (AUS 2020), 318-323. doi: 10.1049/icp.2021.0268.

Wang, M., Gu, W., Wei, L. (2019). Belmon Integrated Aircraft and Propulsion System Simulation for Con-trol and Performance Optimization. 2019 IEEE In-ternational Conference on Mechatronics and Auto-mation (ICMA), 1150-1154. doi: 10.1109/ICMA.2019.8816590.

Kulynych Е., Nazarova, O., Goncharov, D., Chernyshev, S., & Piskun, V. (2020). Laboratory stand with wireless interface for investigation of automatic control systems of DC electric drives. Electrical Engineering and Power Engineering, (3), 24–36. https://doi.org/10.15588/1607-6761-2020-3-3 (in Ukrainian).

Nazarova, O. S., Osadchyy, V. V., Rudim B. Yu. (2023). Research of the microprocessor liquid level automatic control system. Applied Aspects of Information Technology, 6, 2, 163–174. DOI: https://doi.org/10.15276/aait.06.2023.12

Nazarova, O., Osadchyy, V., Shulzhenko, S., Olieinikov M. (2022). Software and Hardware Complex for The Study of Electropneumatic Mechatronic Systems. IEEE 4th International Conference on Modern Electrical and Energy System (MEES), 1-6. doi: 10.1109/MEES58014.2022.10005698.

Sky Brary. Flight Controls, [Electronic resource]. – https://skybrary.aero/articles/flight-controls.

Introduction to aircraft flight controls, [Electronic resource]. – https://www.flightliteracy.com/introduction-to-flight-controls.

Arduino comparison. [Electronic resource]. – Access mode: https://diyi0t.com/technical-datasheet-microcontroller-comparison.

Published

2024-06-27

How to Cite

Nazarova, O., Kulynych, E., & Berezhnyi, O. (2024). A mechatronic system for studying control processes on the example of a "Glide" type aircraft model. Electrical Engineering and Power Engineering, (2), 44–50. https://doi.org/10.15588/1607-6761-2024-2-5

Issue

Section

Automation and computer-integrated technologies