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Influence of the coupling and coherence coefficients in the pitch the flight dynamics of the system «small earth satellite-gurodampers»
- Authors: Kurochkin I.S.1
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Affiliations:
- Institute of the problems of fine mechanics and management, Russian Academy of Science, Saratov
- Issue: Vol 9, No 4 (2010)
- Pages: 65-68
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/944
- DOI: https://doi.org/10.18287/2541-7533-2010-0-4(24)-65-68
- ID: 944
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Abstract
The paper analyses flight dynamics on the basis of coupling and coherence between the parts of a complex dynamic system – small artificial Earth satellite – in the circular orbit using gyroscopic dampers arranged according to the “V-roll” scheme as dampers of their natural oscillations.
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About the authors
I. S. Kurochkin
Institute of the problems of fine mechanics and management, Russian Academy of Science, Saratov
Author for correspondence.
Email: kurochkinis@mail.ru
Post-graduate Student
Russian FederationReferences
- Boyovkin, V. I. Orientation of artificial satellites in gravitational and magnetic fields [Text] / V. I. Boyovkin, Yu. G. Gurevich, Yu. N. Pavlov, G. N. Tolstousov. – Moscow: Science, 1976.
- Kuznetsov, A. Yu. Influence of parametrical perturbations of gyrodampers of the attitude control system of an artificial Earth satellite on its dynamics [Text] / A. Yu. Kuznetsov // Dissertation for the scientific degree of candidate of technical sciences, 2004. 160 p.
- Mandelstamm, L. I. Lectures on the theory of fluctuations [Text] / L. I. Mandelstamm. – M.: Science, 1971. – 160 p.
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