Thermal control of spacecraft star sensor attitude control system based on the solution of a coupled thermoelasticity problem
The paper is devoted to the study of thermal control of the platform of star sensors designed for spacecraft attitude control under operating conditions. An optimal platform design with an arrangement of sensing elements is presented. The temperature field and the stress-strain state of the platform...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Samara National Research University
2016-07-01
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| Series: | Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение |
| Subjects: | |
| Online Access: | https://journals.ssau.ru/vestnik/article/viewFile/3064/3003 |