DocumentCode
3014139
Title
Analysis of the two-chamber shock-absorption system of landing gear based on hybrid methodology
Author
Tomilov, Ivan N. ; Dostovalov, Dmitry N. ; Klokova, Elena A.
Author_Institution
Urga Technol. Inst., Tomsk Polytech. Univ., Tomsk, Russia
fYear
2015
fDate
21-23 May 2015
Firstpage
1
Lastpage
6
Abstract
The paper analyzes complex engineering system - liquid-gas shock-absorption system of landing gear. The system has a combined discrete-continuous behavior. Such systems are called hybrid systems. Simulation is performed in order to improve the control law and minimize the overload effect when landing on the airframe. The analysis is carried out by computer simulation with the use of specialized tools.
Keywords
aircraft instrumentation; gears; shock absorbers; computer simulation; landing gear; liquid-gas shock-absorption system; overload effect; two-chamber shock-absorption system; Absorption; Aircraft; Computational modeling; Electric shock; Gears; Mathematical model; Shock absorbers; behavior map; complex technical system; control law; controlled parameters; discrete-continuous process; event detection; gas-liquid absorption; hybrid system;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Communications (SIBCON), 2015 International Siberian Conference on
Conference_Location
Omsk
Print_ISBN
978-1-4799-7102-2
Type
conf
DOI
10.1109/SIBCON.2015.7147241
Filename
7147241
Link To Document