ON-BOARD CONTROL-MEASUREMENT SYSTEM FOR MICRO CONVERTIPLANE-TYPE UNMANNED AERIAL VEHICLES
Authors
DOI:
https://doi.org/10.31489/2024No2/61-69Keywords:
convertiplane, unmanned aerial vehicles, on-board control-measurement system, accelerometer, gyroscope, diagnosis, thermometerAbstract
Abstract. The article describes the on-board control-measurement system designed to record the main flight parameters of a micro-convertiplane type unmanned aerial vehicle and the element base used for this purpose. The methodology of conducting tests in stationary mode through the on-board control-measurement system was developed and tests were carried out. The engine's diagnostic check and condition assessment has been performed using the on-board control-measuring system. The possibility of on-ground check of the micro unmanned aerial vehicles power elements before and after the flight, as well as the possibility of monitoring the flight events that may occur in the air during the flight has been shown. The data on the power consumption and temperature of each engine in the stationary mode, the direction of the aircraft axes and the velocity vector have been recorded by mean of the developed on-board control-measurement system, as well as time dependence diagrams of the corresponding parameters have been built in comparative order based on the obtained values. A methodology has been developed for the diagnostics of the engine operation of the micro-unmanned aerial vehicle before and during the flight. It has been shown that the temperature, power consumption and number of revolutions of the engines included in the power system of the aircraft, as well as the aircraft axes and velocity vector direction data is recorded during the flight, by mean of the on-board control-measurement system designed to collect data on the flight-technical parameters of the convertiplane-type micro-unmanned aerial vehicles.
References
Nabiyev R.N., Abdullayev A.A., Qarayev Q.I., Abbasov V.A. (2022) Determination of the center of gravity of an unmanned aerial vehicle of a tiltrotor type. Izvestiya SFedU. Engineering Sciences, 229, 5, 258 – 268. [in Russian] DOI: 10.18522/2311-3103-2022-5-258-268. DOI: https://doi.org/10.18522/2311-3103-2022-5-258-268
Nabiyev R.N., Qarayev Q.I., Abdullayev A.A. (2020) Conceptual functional design of hybrid energy source of unmanned convertiplane. Proceedings of the IOP Conference Series: Conference Scopus. Materials Science and Engineering. 862, 022043. DOI: 10.1088/1757-899X/862/2/022043. DOI: https://doi.org/10.1088/1757-899X/862/2/022043
Mikhaylov S.A., Khamza M.A.K., Makhanko A.A. (2023) Method for determınıng aırcraft aerodynamıc characterıstıcs based on flıght experıment results. Patent – Invention, RU 2790358 С1. Federal servıce for ıntellectual property,Russian Federation. No.5, Publ.17.02.2023. Available at: https://patents.google.com/patent/RU2790358C1/ru
Emelyanova O.V., Kazaryan K.G., Martinez Leon A.S., Jatsun S.F. (2017) The synthesis of electric drives characteristics of the UAV of “convertiplane - tricopter” type. Cloud of Science. 4, 2, 249–263. [in Russian].Available at: http://cloudofscience.ru DOI: https://doi.org/10.1051/matecconf/20179902002
Khamza M.A.K. (2023) Designing a flight information collection system for calculating the aerodynamic charac-teristics of a UAV. Ontology of Designing. 13, 1, 93 – 98. DOI: 10.18287/2223-9537-2023-13-1-90-98. DOI: https://doi.org/10.18287/2223-9537-2023-13-1-90-98
Kleshnina S.A., Kleshnin V.YU., Boev N.M., Krilov E.D. (2018) Device for recording and transmitting telemetric information of an unmanned aerial vehicle.Patent RU 182090 С1, No. 22, Publ. 2018.08.03. Available at: https://patents.google.com/ patent/RU182090U1/ru
Kuat К.İ. (2022) Determination of aerodynamic characterisitcs of fixed-wing unmanned aerial vehicle by analytical techniques.Tomsk State University Journal of Mathematics and Mechanics, 78, 112 – 124. [in Russian]. DOI: 10.17223/1998821/78/9. DOI: https://doi.org/10.17223/19988621/78/9
Nabiyev R.N., Abdullayev A.A., Garayev Q.I. (2024) Study of flıght-technıcal parameters of convertoplan-type unmanned mıcro aırcraft ın multıcopter mode. Scientific Journal National Aviation Academy. 26, 1, 17 – 29. [in Azerbaijani]. Available at: https://scientific-journals.naa.edu.az:8070/articles/get/62
Alkahdery L.A., Yurchenko A.V., Mohammed J.A.-K., Neshina Y.G. (2023) Automated temperatureand humidity control and monitoring system for improving the performance in drying system. Eurasian Physical Technical Journal. 20, 2(44), 32 – 40. DOI: 10.31489/2023No2/32-40 DOI: https://doi.org/10.31489/2023No2/32-40
Downloads
Received
Revised
Accepted
Published online
How to Cite
Issue
Section
License
This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
