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A system of compensating rotary microacceleration by a magnetic method
- Authors: Syomkin N.D.1, Balakin V.L.1, Voronov K.Y.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 6, No 1 (2007)
- Pages: 64-80
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/479
- DOI: https://doi.org/10.18287/2541-7533-2007-0-1(12)-64-80
- ID: 479
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Abstract
The paper deals with a system that uses a magnetic method of compensating microaccelerations and does not require changing the design of a space vehicle (SV). The results of modelling the motion relative to the centre of mass for different types of SV are given.
About the authors
N. D. Syomkin
Samara State Aerospace University
Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation
V. L. Balakin
Samara State Aerospace University
Email: sadohina@ssau.ru
Russian Federation
K. Ye. Voronov
Samara State Aerospace University
Email: sadohina@ssau.ru
Russian Federation
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