The question of adaptive control of the aviation engine in the absence of its mathematical description with application of neural technology on examples of regulation of temperature of gases behind the turbine of low pressure and regulation of frequency of rotation of a rotor of the fan is considered. It is shown that both parameters of the aviation engine both in a statics and in dynamics meet the requirements of technical operation.

aviation engine, adaptive management, neural technology

1. Sinyakov A.N., Shaymardanov F.A. Sistemy avtomaticheskogo upravleniya letatel’nymi apparatami i ich silovymi ustanovkami [Systems of Automatic Control of Aircarfts and their Power Devices]. Moscow, Mashinostroenie Publ., 1991, 320 p.
2. Antonov V. N., Terechov V.A., Tyukin I.Yu. Adaptivnoe upravlenie v technichskich sistemach. Uchebnoe posobie [Adaptive Control in Technical Systems. Manual]. SPb.: ShBU Publ., 2001, 244 p.
3. Legotkina T.S. Danilova S. A. Metody identifikatsii sistem [Methods of System Identification]. Perm;, Perm GSU Publ., 2008, pp. 48–50.