Influence of the coupling and coherence coefficients in the pitch the flight dynamics of the system «small earth satellite-gurodampers»

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.

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 Federation

References

  1. 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.
  2. 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.
  3. Mandelstamm, L. I. Lectures on the theory of fluctuations [Text] / L. I. Mandelstamm. – M.: Science, 1971. – 160 p.

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