Email this article Method for Validation of the Onboard Attitude Control System Software of the Auriga Earth Remote Sensing Small Spacecraft
- Authors: Rozin P.E.1
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Affiliations:
- Dauria Aerospace, Skolkovo
- Issue: Vol 51, No 7 (2017)
- Pages: 646-653
- Section: Article
- URL: https://journal-vniispk.ru/0038-0946/article/view/170899
- DOI: https://doi.org/10.1134/S0038094617070164
- ID: 170899
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Abstract
The paper considers a digital modeling complex for the attitude control system of the Auriga Earth remote sensing small spacecraft. Mathematical models of measuring and executive devices are described. The results of spacecraft orbital attitude tests are presented.
About the authors
P. E. Rozin
Dauria Aerospace, Skolkovo
Author for correspondence.
Email: info@dauria.ru
Russian Federation, Moscow oblast
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