Quadcopter Hydraulic Drive as an Object of Regulation
- Authors: Tselishchev V.A.1
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Affiliations:
- Ufa University of Science and Technology
- Issue: No 2 (2025)
- Pages: 6-25
- Section: Problems, prospects for the development and application of unmanned aircraft systems
- URL: https://bakhtiniada.ru/2312-1327/article/view/305984
- DOI: https://doi.org/10.51955/2312-1327_2025_2_6
- ID: 305984
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Full Text
Abstract
The features of the development of domestic unmanned aerial vehicles are given. The main problems of the technological evolution of cargo quadrocopters have been revealed. The concept of the development of unmanned cargo multi-purpose multi-propeller flying aircraft is presented, reflecting the system of using a hydraulic transmission using the example of a quadcopter. The issues of accuracy, stability, controllability of the automatic control system and regulation of the hydraulic transmission of a cargo quadcopter are considered. A possible description of the hydraulic drive of the quadrocopter rotors as an object of regulation is presented. The forces acting on the quadcopter in flight have been determined. The controlling, disturbing and corrective effects on the automatic control and regulation system of the hydraulic transmission of the quadcopter are identified and described. The analysis of the possibility of using aircraft piston engines to drive the transmission of a cargo quadcopter, volumetric axial plunger pumps and hydraulic motors has been performed. New circuit solutions for hydromechanical devices for correcting static and dynamic characteristics are shown. Schematic solutions of hydraulic transmission regulators are presented: pressure regulator, dynamic pressure regulator, speed regulator, power regulator, LS regulator. The advantages of using regulators are described. The proposed hydro–mechanical controller with LS-regulation makes it possible to improve flight stability and energy efficiency of a multi-rotor aircraft.
About the authors
V. A. Tselishchev
Ufa University of Science and Technology
Author for correspondence.
Email: pgl.ugatu@mail.ru
Doctor of Technical Sciences, Professor 32, Zaki Validi street, Ufa, 450076, Russia
References
- Berger T., Tischler M. B., Horn J. F. (2012). High-Speed Rotorcraft Pitch Axis Response Type Investigation. VFS International 77th Annual Forum & Technology Display. West Palm Beach, Florida. doi: 10.4050/F-0077-2021-16793
- Gabuev K. O., Kucherenko N. A., Shipko A. I. (2018). The automatic control system of an unmanned aerial vehicle. Automation Technological and Business Processes. 10(4). doi: 10.15673/atbp.v10i4.821. (In Russian)
- Kava S. A. (2016). Dynamics and Control of a Multi-Rotor Aircraft. 20th Australasian Fluid Mechanics Conference Perth, Australia 5-8 December.
- Kuderko D. A., Polyakov N. A., Frolov G. K., Tselishchev V. A. (2024). High-speed power transmission unit with hydromechanical control. Bulletin of the Perm National Research Polytechnic University. Aerospace engineering. 76: 30-40. doi: 10.15593/2224-9982/2024.76.03. (In Russian)
- Margun A. A., Zimenko K. A., Bazylev D. N. (2014). A control system for an unmanned aerial vehicle equipped with a robotic arm. Scientific and Technical Bulletin of Information Technologies, Mechanics and Optics. 6(94): 54-62. (In Russian)
- Patent No. 205086 U1 Russian Federation, IPC B64C 27/12, B64D 35/04. Hydraulic drive of a screw aircraft : No. 2021103965 : application 02/16/2021 : published 06/28/2021 / V. A. Tselishchev, I. S. Khakimov ; applicant Federal State Budgetary Educational Institution of Higher Education Ufa State Aviation Technical University. EDN GIQWAM.
- Patent No. 2808657 C1 Russian Federation, IPC B64D 35/04, B64C 27/12. Hydraulic drive of a multi-rotor aircraft: No. 2023110764 : application 04/26/2023 : published 11.30.2023 / V. A. Tselishchev, D. V. Tselishchev, I. S. Khakimov ; applicant Federal State Budgetary Educational Institution of Higher Education Ufa University of Science and Technology. Utility Model
- Polyakov N. A., Solovyova A. A., Tselishchev V. A. (2021). The concept of the development of power transmission units in the hydraulic system of a civil aircraft. Bulletin of the Perm National Research Polytechnic University. Aerospace engineering. 67: 5-15. doi: 10.15593/2224-9982/2021.67.01. (In Russian)
- Saetti U., Guner F. (2024). Interactional Aerodynamics Modeling and Flight Control Design of Multi-Rotor Aircraft. February 2024. Conference: 6th Decennial VFS Aeromechanics Specialists' Conference At: Santa Clara, CA.
- Saetti U., Horn J. F. (2022). Flight Dynamics and Control of an eVTOL Concept Aircraft with Propeller-Driven Rotor. Journal of the American Helicopter Society. 67. doi: 10.4050/JAHS.67.03201226.
- Scaramal M., Horn J. F., Saetti U. (2021). Load Alleviation Control using Dynamic inversion with DirectLoad Feedback. VFS International 77th Annual Forum & Technology Display. West Palm Beach, Florida.
- Shastry A., Gessow A. (2020). Predicting Wake and Structural Loads in RPM Controlled Multirotor Aircraft. Conference: TVF F/2020At: San Jose, California. 575-590.
- Tselishchev V. A. (2022). Calculation and design of a volumetric hydraulic drive. Ufa : UGATU. 2022. 216. (In Russian)
- Vikulov O. V. (2023). Promising helicopter-type unmanned aerial vehicles of domestic production. Innovation and expertise: scientific papers. 1(35): 70-82. (In Russian)
- Zhu Yu. (2022). A model of an unmanned aerial vehicle (quadcopter) control system. Computer Science, telecommunications and management. 15(3): 49-61. doi: 10.18721/JCSTCS.15304.
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