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

Bibliographic Details
Parent link:MATEC Web of Conferences
Vol. 48 : Space Engineering.— 2016.— [01005, 6 p.]
Main Author: Dmitriev V. S. Viktor Stepanovich
Corporate Author: Национальный исследовательский Томский политехнический университет
Other Authors: 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.
Language:English
Published: 2016
Series:Spacecrafts and Devices
Subjects:
Online Access:http://dx.doi.org/10.1051/matecconf/20164801005
http://earchive.tpu.ru/handle/11683/33712
Format: Electronic Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=648911
Description
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.
DOI:10.1051/matecconf/20164801005