Integrated approach of the dynamic characteristics optimization for spacecraft’s technical systems on the exploratory tests; MATEC Web of Conferences; Vol. 48 : Space Engineering

Integrated approach of the dynamic characteristics optimization for spacecraft’s technical systems on the exploratory tests; MATEC Web of Conferences; Vol. 48 : Space Engineering

Detalles Bibliográficos
Parent link:MATEC Web of Conferences
Vol. 48 : Space Engineering.— 2016.— [01005, 6 p.]
Autor Principal: Dmitriev V. S. Viktor Stepanovich
Autor Corporativo: Национальный исследовательский Томский политехнический университет
Outros autores: Britova Yu. A. Yuliya Aleksandrovna
Summary:Title screen
Integrated approach is the process connecting various project, theoretical and testing procedures. It is provided by the specific series-parallel combination of the mentioned operations. This paper shows that using results of the previous procedures on the further algorithm stages of exploratory tests and product verification is expedient. At that, the necessary correcting of engineering solutions in corresponding procedures is conducted simultaneously. Then, results of each procedure are used in the fixed sequence. It provides maximum attainable optimality of the designed system.
Idioma:inglés
Publicado: 2016
Series:Spacecrafts and Devices
Subjects:
электронный ресурс
труды учёных ТПУ
интегрированный подход
оптимизация
динамические характеристики
космические аппараты
Acceso en liña:http://dx.doi.org/10.1051/matecconf/20164801005
http://earchive.tpu.ru/handle/11683/33712
Formato: Electrónico Capítulo de libro
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=648911

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