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Differential parameter method of aircraft flight simulation in aviation virtual electronic proving grounds
Author(s) -
А. Р. Бестугин,
A D Filin,
И. А. Киршина
Publication year - 2020
Publication title -
iop conference series. materials science and engineering
Language(s) - English
Resource type - Journals
eISSN - 1757-899X
pISSN - 1757-8981
DOI - 10.1088/1757-899x/862/5/052061
Subject(s) - aviation , set (abstract data type) , differential (mechanical device) , aerospace engineering , flight simulator , computer science , differential equation , euler's formula , path (computing) , simulation , engineering , mathematics , mathematical analysis , programming language
The study has been carried out to justify and choose an optimal method of aircraft flight simulation when designing virtual electronic proving grounds. A differential parameter method and algorithm of a set aircraft flight path simulation has been proposed based on the target status word assignment corresponding to each simulated aircraft and the joint implementation of a set of Euler’s dynamical equations.

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