Open AccessInformation flows of parallel computing of the distributed control systems of aviation engines
Author(s) -
Serhii Tovkach
Publication year - 2021
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1891/1/012054
Subject(s) - computer science , aviation , control (management) , work (physics) , generator (circuit theory) , information exchange , control engineering , systems engineering , distributed computing , engineering , aerospace engineering , mechanical engineering , telecommunications , power (physics) , physics , quantum mechanics , artificial intelligence
The ongoing work on scientific and technical suggestions for 6 th generation engines has been considered and the necessity for developing methods for constructing adaptive control of aircraft engines has been substantiated, which will allow, due to the flexible structure of the control system, to determine the number of adjustable parameters and the number of adjustable factors for the formation of engine control programs. The information flows of aircraft engine control systems have been analyzed using an example of a system with full responsibility of the FADEC type and a method for their parallel calculations is proposed, for the implementation of which it is necessary to develop a virtual channel model, a background stream generator, and a data parallelization method.