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 :
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