| Issue |
MATEC Web of Conferences
Volume 48, 2016
IV Russian Forum for Young Scientists with International Participation “Space Engineering”
|
|
|---|---|---|
| Article Number | 01005 | |
| Number of page(s) | 6 | |
| Section | 1. Spacecrafts and Devices | |
| DOI | https://doi.org/10.1051/matecconf/20164801005 | |
| Published online | 04 April 2016 | |
Integrated approach of the dynamic characteristics optimization for spacecraft’s technical systems on the exploratory tests
National Research Tomsk Polytechnic University, 634050 Tomsk, Russia
a Corresponding author : dmitriev@tpu.ru
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.
© Owned by the authors, published by EDP Sciences, 2016
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