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

Detalhes bibliográficos
Parent link:	Control and Communications (SIBCON).— 2015.— [6 p.]
Autor principal:	Tomilov I. N. Ivan Nikolaevich
Autor Corporativo:	Национальный исследовательский Томский политехнический университет (ТПУ) Юргинский технологический институт (филиал) (ЮТИ) Кафедра информационных систем (ИС)
Outros Autores:	Dostovalov D. N. Dmitry Nikolaevich, Klokova E. A. Elena Aleksandrovna
Resumo:	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:	inglês
Publicado em:	2015
Assuntos:	электронный ресурс труды учёных ТПУ
Acesso em linha:	http://dx.doi.org/10.1109/SIBCON.2015.7147241
Formato:	Recurso Electrónico Capítulo de Livro
KOHA link:	https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=647363

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