Open AccessMethods and Algorithms of Turbojet Engines Thrust Parameters Control Unerroric
Author(s) -
Adeliya Yu. Burova
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 - 10.1088/1742-6596/2096/1/012060
Subject(s) - turbojet , thrust , computer science , rotor (electric) , control (management) , control engineering , algorithm , engineering , aerospace engineering , mechanical engineering , artificial intelligence
This report shows a real way for solving the problem of turbojet engine thrust parameters control in flight. The purpose of the research is the formalization of the digital methods and its algorithms for turbojet engines thrust parameters control unerroric. The methods of deductive digital signal processing and combined method of system analysis and approximate synthesis are used for such research. It is described the digital algorithms of unerroric methods wich are based on rotor speed control for turbojet engines of twin-engine airliner by its power plant control system. There are given the calculation formulas for those algorithms.