FUZZY AUTOMATIC CONTROL SYSTEM SYNTHESIS OF THE PROPELLER FAN THE AVIATION GAS TURBINE ENGINE
DOI:
https://doi.org/10.18372/1990-5548.58.13510Keywords:
Automatic control system, aviation gas turbine engine, fuzzy regulator, propeller fan, harmonic linearizationAbstract
The article deals with the method of automatic control systems synthesis of with a fuzzy controller, which is considered as a separate subsystem within the general control system. Due to the use of the harmonic linearization method, the research of the electronic control system according to the given index of oscillation has been carried out and the fuzzy control system of the aviation engine fan propeller has been designed. Through the simulation, the dependences of the quality the transient process on the parameters of the membership functions for closed systems with fuzzy PI- and PD-regulators were revealed; detected dependencies can be used to form the base rules expert system to configure the regulator from the condition of fulfilling the specified quality criteria.
References
A. N. Melikhov, L. S. Bernstein, and S. Ya. Korovin, Fuzzy logic situational advisory systems, Nauka, 1990, 272 p. (in Russian)
B. Bica, G. Akat, A. J. Khipperfield and P. J. Fleming, “Multiobjective Design of a Fuzzy Controller for a Gas Turbine Aero-Engine,” Proceedings of UKACC Int Conf on CONTROL'98, 455, pp. 901–906.
I. M. Makarov and V. M. Lokhin, Intelligent automatic control systems, FIZMATLIT, 2001, 576 p. (in Russian).
K. Asai, D. Watada, and S. Iwai, Applied fuzzy systems, Mir, 1993, 368 p. (in Russian)
L. A. Zadeh, “Fuzzy Logic, Neural Networks, and Soft Computing,” II Fuzzy Systems, 37(3), 1994, pp. 77–84. https://dl.acm.org/citation.cfm?id=175255
S. V. Enchev and O. V. Pavelko, “Dynamic Synthesis of a Linux System of the Two-Way System of Controlling the of the propeller fan TGVD D-27,” Science technology, 2013, 4 (16), pp. 14–19. (in Ukrainian)
S. V. Enchev and S. S. Tovkach, “The use of fuzzy logic for processing information in electronic control systems of aircraft engines,” Proceedings of the 5nd International Conference MINTT-2013, 1, pp. 55–58. (in Ukrainian).
S. V. Enchev, S. S. Ilyenko, and K. N. Gavrenko, “Dynamic model of the automatic propulsion system of the aircraft engine,” Proceedings of the 1st International Conference MINTT-2009, 3, pp. 9–13. (in Ukrainian)
V. I. Vasilyev and B. Kh. Ilyasov, Intelligent control systems using fuzzy logic, USATU, 1995, 100 p.(in Russian)
V. V. Panin, S. V. Enchev, and S. A. Taku, “Formation of the structure of the intellectual system of automatic control of aviation gas turbine engines,” Aerospace techniques and technology. 2013, 7(104). pp. 181–185. (in Ukrainian)
Downloads
Issue
Section
License
Authors who publish with this journal agree to the following terms:
Authors retain copyright and grant the journal right of first publication with the work simultaneously licensed under a Creative Commons Attribution License that allows others to share the work with an acknowledgement of the work's authorship and initial publication in this journal.
Authors are able to enter into separate, additional contractual arrangements for the non-exclusive distribution of the journal's published version of the work (e.g., post it to an institutional repository or publish it in a book), with an acknowledgement of its initial publication in this journal.
Authors are permitted and encouraged to post their work online (e.g., in institutional repositories or on their website) prior to and during the submission process, as it can lead to productive exchanges, as well as earlier and greater citation of published work (See The Effect of Open Access).