Analysis of the two-chamber shock-absorption system of landing gear based on hybrid methodology; Control and Communications (SIBCON)

Dades bibliogràfiques
Parent link:Control and Communications (SIBCON).— 2015.— [6 p.]
Autor principal: Tomilov I. N. Ivan Nikolaevich
Autor corporatiu: Национальный исследовательский Томский политехнический университет (ТПУ) Юргинский технологический институт (филиал) (ЮТИ) Кафедра информационных систем (ИС)
Altres autors: Dostovalov D. N. Dmitry Nikolaevich, Klokova E. A. Elena Aleksandrovna
Sumari: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
Idioma:anglès
Publicat: 2015
Matèries:
Accés en línia:http://dx.doi.org/10.1109/SIBCON.2015.7147241
Format: Electrònic Capítol de llibre
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=647363
Descripció
Sumari: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