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

Dettagli Bibliografici
Parent link:Control and Communications (SIBCON): International Siberian Conference on Russia, Omsk, May 21-23, 2015. [6 p.].— , 2015
Autore principale: Tomilov I. N. Ivan Nikolaevich
Ente Autore: Национальный исследовательский Томский политехнический университет (ТПУ) Юргинский технологический институт (филиал) (ЮТИ) Кафедра информационных систем (ИС)
Altri autori: Dostovalov D. N. Dmitry Nikolaevich, Klokova E. A. Elena Aleksandrovna
Riassunto: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
Pubblicazione: 2015
Soggetti:
Accesso online:http://dx.doi.org/10.1109/SIBCON.2015.7147241
Natura: Elettronico Capitolo di libro
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=647363

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