Analysis of the two-chamber shock-absorption system of landing gear based on hybrid methodology

Analysis of the two-chamber shock-absorption system of landing gear based on hybrid methodology

Bibliographic Details
Parent link:Control and Communications (SIBCON): International Siberian Conference on Russia, Omsk, May 21-23, 2015. [6 p.].— , 2015
Main Author: Tomilov I. N. Ivan Nikolaevich
Corporate Author: Национальный исследовательский Томский политехнический университет (ТПУ) Юргинский технологический институт (филиал) (ЮТИ) Кафедра информационных систем (ИС)
Other Authors: Dostovalov D. N. Dmitry Nikolaevich, Klokova E. A. Elena Aleksandrovna
Summary:Title screen
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.
Режим доступа: по договору с организацией-держателем ресурса
Published: 2015
Subjects:
электронный ресурс
труды учёных ТПУ
Online Access:http://dx.doi.org/10.1109/SIBCON.2015.7147241
Format: Electronic Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=647363
Description
Summary:Title screen
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.
Режим доступа: по договору с организацией-держателем ресурса
DOI:10.1109/SIBCON.2015.7147241

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