Author(s):
1. ADELIYA BUROVA:
Moscow Aviation Institute (National Research University), Moscow, Russian Federation
2. ANATOLY RYAPUKHIN:
Moscow Aviation Institute (National Research University), Moscow, Russian Federation
Abstract:
This article shows a good idea to digitalize any unerrorics for software of turbojet engine thrust asymmetry control. The well-known results of scientific developments presented in the publications used confirm the practical usefulness and relevance of digitalization of measurement results processing methods for the software unerroric of applied algorithms for system analysis and approximate synthesis. However, the equality of addition and multiplication speeds in digital signal processors and programmable logical devices is achieved mainly by hardware. Therefore, the need to reduce hardware costs for digital signal processing increases the role of IT-research on the possibility of flight safety analytics by software. The article purpose is a research of software for unerroric of such control. The used methods of that research are the methods of system analysis and the methods of the software modeling. To achieve the stated goal, the following tasks have been set and solved: the task of directional search and comparative evaluation of digital methods for ensuring unerroric of control of mutual compliance of controlled values of thrust parameters of two-shaft turbojet two-circuit engines of the same series; the task of adapting deductive algorithms for digital processing of measurement results of controlled values of thrust parameters of twoshaft turbojet two-circuit engines for the software of an unerroric of the flight of a twin-engine aircraft with such engines; the task of selecting the element base for hardware and software experimental modeling of digital algorithms for software unerroric of thrust asymmetry of turbojet two-circuit engines. The formulation and solution of problems of selection and adaptation of methods and algorithms for digital processing of measurement results contributed to the development of software for flight safety unerroric of a twin-engine airliner with twin-shaft turbojet engines by tightening the control of the mutual correspondence of the controlled values of their thrust parameters. The results of experimental modeling of adapted algorithms have confirmed the practical feasibility of such software and the high importance of ITresearch in its design. It is described the possibility of turbojet two-circuit engines tractions forces asymmetry analysis unerroric. A set of formulas for digital processing of control signals from rotors speeds sensors of civil airplane with two turbojet two-circuit engines is presented.
Page(s):
6482-6489
DOI:
DOI not available
Published:
Journal: Journal of Theoretical and Applied Information Technology, Volume: 100, Issue: 21, Year: 2022
Keywords:
Quality
,
Engine
,
Thrust
,
Unerroric
,
Airliner
References:
References are not available for this document.
Citations
Citations are not available for this document.