Authors | S.S. Tovkach |
Affiliations |
National Aviation University, Lubomyr Husar Avenue, 1, 03058 Kyiv, Ukraine |
Е-mail | |
Issue | Volume 12, Year 2020, Number 1 |
Dates | Received 11 November 2019; revised manuscript received 15 February 2020; published online 25 February 2020 |
Citation | S.S. Tovkach, J. Nano- Electron. Phys. 12 No 1, 01003 (2020) |
DOI | https://doi.org/10.21272/jnep.12(1).01003 |
PACS Number(s) | 02.50.Ng, 87.63.L |
Keywords | Liebman process, Aviation engine, Electronic control system, Information flows, Distributed system, Elliptical equations, Computing templates, Visualization. |
Annotation |
The paper describes the Liebman process of creating distributed and reliable ACS aircraft power plant within the identifying information flows in the interaction of nodes, which allows, on the one hand, to organize optimal control with adaptation to changing external conditions and, on the other hand, to take timely and correct decisions when violations occur in the power plant or in the control part of the ACS. In the case of the distributed information flows of the electronic control system of aviation engine, different equation techniques have been considered and, depending on the given part of the system, their useful types have been defined: elliptical, hyperbolic, parabolic. According to the Liebman averaging process the practical iteration with the sufficient number of special computing templates has been proposed for estimating the accuracy of the grid-derived solution of the distributed information flow of the engine automatic control system. The scheme of the information flow processing of the electronic system based on the developed algorithm and practical results in the form of programming language and graph visualization has been presented. |
List of References |