Organization of Distributed Information Systems the Aviation Gas Turbine Engine

UDC 681.51:621.452.3(045) DOI:10.18372/1990-5548.61.14210

S. S. Tovkach. Organization of Distributed Information Systems the Aviation Gas Turbine Engine // Electronics and Control Systems, N 3(61) – Kyiv: NAU, 2019. – pp. 29–35.

The article deals with the method of distributed information systems organization the aviation engine, which is considered as a interaction of the components of the automatic control system in its technological activity. Due to the use of the ZigBee interface communication, the research of the electronic control system according to the given index of transitive packet has been carried out and the distributed control system usage of the aviation engine has been proposed. Through the simulation, the dependences of the quality the transmission packet request on the parameters of the maximum flow the distributed net for closed systems with switching bandwidth were revealed; detected dependencies can be used to form a mathematical model of replacing two-way flow and one-way flow information transmission to configure gas turbine engine distributed net from the condition of fulfilling the specified switching bandwidth.

Index Term—automatic control system; aviation gas turbine engine; distributed system; nets models; bandwidth.
References: 10 names.