Open AccessResearch on Air Flight Simulation Control Law of Large Aircraft
Author(s) -
Junbin You
Publication year - 2020
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 - 10.1088/1742-6596/1678/1/012032
Subject(s) - rudder , aileron , stability derivatives , elevator , throttle , control theory (sociology) , variable (mathematics) , flight simulator , stability (learning theory) , electronic stability control , engineering , control variable , aircraft flight mechanics , flight control surfaces , law , trajectory , control engineering , computer science , aerodynamics , simulation , control (management) , aerospace engineering , automotive engineering , mathematics , physics , mathematical analysis , astronomy , artificial intelligence , machine learning , political science
The air flight simulator, also known as the variable stability aircraft, can make the dynamic characteristics of the machine change or simulate the response characteristics of different objects in a large range through the variable stability telex system. This paper is devoted to the research of the air flight simulation control law of large aircraft, and designs the five degree of freedom variable stability control law: to control the elevator, rudder and aileron of the basic aircraft, and to design the three-degree-of-freedom variable stability control law. The control of the direct lift surface and the automatic throttle was added, and the five-degree-of-freedom variable stability control law was designed to simulate the trajectory characteristics and velocity characteristics. Finally, the variable stability control law is verified based on the target aircraft simulator.