| Autor: |
A.N. Pavlov, A.Yu. Kylakov, V.N. Vorotyagin, A.B. Umarov |
| Rok vydání: |
2020 |
| Předmět: |
|
| Zdroj: |
Informatization and communication. 5:132-140 |
| ISSN: |
2078-8320 |
| DOI: |
10.34219/2078-8320-2020-11-5-132-140 |
| Popis: |
At the stages of design, creation and application of small spacecraft to develop solutions aimed at increasing their stability, it is necessary to assess the indicators of structural and functional reliability of elements of onboard systems, taking into account the involvement of various modes of operation. This article presents the results of a study of the influence of confi gurations of sensors of the attitude control system on the structural and functional reliability of a small spacecraft when solving task of determining the attitude in various modes of operation. |
| Databáze: |
OpenAIRE |
| Externí odkaz: |
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