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

Détails bibliographiques
Parent link:	Control and Communications (SIBCON): International Siberian Conference on Russia, Omsk, May 21-23, 2015. [6 p.].— , 2015
Auteur principal:	Tomilov I. N. Ivan Nikolaevich
Collectivité auteur:	Национальный исследовательский Томский политехнический университет (ТПУ) Юргинский технологический институт (филиал) (ЮТИ) Кафедра информационных систем (ИС)
Autres auteurs:	Dostovalov D. N. Dmitry Nikolaevich, Klokova E. A. Elena Aleksandrovna
Résumé:	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
Publié:	2015
Sujets:	электронный ресурс труды учёных ТПУ
Accès en ligne:	http://dx.doi.org/10.1109/SIBCON.2015.7147241
Format:	Électronique Chapitre de livre
KOHA link:	https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=647363

Internet