Integrated approach of the dynamic characteristics optimization for spacecraft’s technical systems on the exploratory tests

Opis bibliograficzny
Parent link:MATEC Web of Conferences
Vol. 48 : Space Engineering.— 2016.— [01005, 6 p.]
1. autor: Dmitriev V. S. Viktor Stepanovich
Korporacja: Национальный исследовательский Томский политехнический университет
Kolejni autorzy: Britova Yu. A. Yuliya Aleksandrovna
Streszczenie: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.
Język:angielski
Wydane: 2016
Seria:Spacecrafts and Devices
Hasła przedmiotowe:
Dostęp online:http://dx.doi.org/10.1051/matecconf/20164801005
http://earchive.tpu.ru/handle/11683/33712
Format: Elektroniczne Rozdział
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=648911

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