Characteristics analysis and drive type selection for aileron control of a heavy unmanned aerial vehicle
Authors: Radetskaya A.A. | |
Published in issue: #10(75)/2022 | |
DOI: 10.18698/2541-8009-2022-10-833 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control |
|
Keywords: heavy unmanned aerial vehicle, ailerons, electromechanical drive, electrohydraulic drive, autopilot, characteristics, steering surface |
|
Published: 22.11.2022 |
Aircraft rudder actuators form part of the aircraft rudder control system, which ensures both piloting of the aircraft by the pilot and automatic flight of the aircraft along the specified trajectories, therefore the task of choosing the required actuator for aileron control of the aircraft is an integral stage in the design of the lateral control channel and requires consideration of many parameters and computational data. The present work is devoted to analyzing the characteristics and selecting the type of actuator for aileron control of a heavy unmanned aerial vehicle. Choosing the right type of aileron control actuator solves a number of fundamental engineering problems when creating an autopilot system and a comprehensive control system for an unmanned aerial vehicle.
References
[1] Ermakov S.A., Karev V.I., Mitrichenko A.N. et al. Control actuation systems of civil aircraft. New developments and reliability. Vestnik MAI [MAI Aerospace Journal], 2010, vol. 17, no. 3. URL: https://vestnikmai.ru/publications.php?ID=23441 (in Russ.).
[2] Batishchev D.V., Gummel A.A., Gilmiyarov K.R. Electro-mechanical drive for aileron aircraft. Izvestiya vysshikh uchebnykh zavedeniy. Severo-Kavkazskiy region. Tekhnicheskie nauki [Bulletin of Higher Educational Institutions. North Caucasus Region. Technical Sciences], 2013, no. 1, pp. 74–78 (in Russ.).
[3] Raznitsa mezhdu elektricheskimi, pnevmaticheskimi i gidravlicheskimi lineynymi privodami [Difference between electric, pneumatic and hydraulic linear drives]. engineering-solutions.ru: website (in Russ.). URL: https://engineering-solutions.ru/motorcontrol/actuator_linear/ (accessed: 29.05.2022).
[4] Mikhalev I.A. Okoemov B.N., Chikulaev M.S. Sistemy avtomaticheskogo upravleniya samoletom [Automatic control systems of aircraft]. Moscow, Mashinostroenie Publ., 1987 (in Russ.).
[5] Kuznetsov S.V., Gusev A.A. Metodicheskie ukazaniya po izucheniyu distsipliny “Sistemy avtomaticheskogo upravleniya poletom” [Methodological instructions for the study of “Automatic flight control systems discipline”]. Moscow, MGTU GA Publ., 2004 (in Russ.).
[6] Kiriakidi S.K., Satin V.A. Proektirovanie samoletov [Aircraft design]. Moscow, VGTU Publ., 2009 (in Russ.).
[7] Vorobyev V.G., Kuznetsov S.V. Avtomaticheskoe upravlenie poletom samoletov [Automatic aircraft flight control]. Moscow, Transport Publ., 1995 (in Russ.).
[8] Vorobyev V.V., Gritsenko N.A., Nikolaev Yu.A. et al. Sistemy samoleta i dvigatelya. Sistemy vertoleta i dvigatelya [Aircraft and engine systems. Helicopter and engine systems]. Moscow, MGTU GA Publ., 2015 (in Russ.).