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Orientation of Large Orbital Stations

  • V. A. Sarychev
  • M. Yu. Belyaev
  • V. V. Sazonov
  • T. N. Tyan
Conference paper
Part of the International Union of Theoretical and Applied Mechanics book series (IUTAM)

Abstract

The single-axis gravitational orientation mode is considered for the Salyut 6 and 7 orbital stations. An integral statistical technique is described for determining the real rotational motion of the stations in this mode by the solar and magnetic sensor indications. The technique is illustrated by computations of residual microaccelerations aboard the station; their knowledge is important for an analysis of some technological experiments.

Keywords

Station Motion Versus Versus Versus Versus Aerodynamic Drag Orbital Station Attitude Motion 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

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    Sazonov, V.V.; Belyaev, M.Yu.; Kuz’min, S.P.; Tyan, T.N.: Investigation of an accuracy in determining the rotational motion of Salyut 6 and Salyut 7 orbital stations in the gravitational orientation mode by using measurement data. Preprint, Keldysh Inst. Appl. Math., USSR Ac. Sci. (1986), N 192.Google Scholar
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    Sarychev, V.A.; Sazonov, V.V.; Belyaev, M.Yu.; Efimov, N.I.; Tyan, T.N.; Sheffer, E.K.; Sklyankin, V.A.: Specifying the rotational motion of the Salyut 7 orbital station by using the star photometer indications. Preprint, Keldysh Inst. Appl. Math., USSR Ac. Sci. (1987), N 233.Google Scholar

Copyright information

© Springer-Verlag Berlin Heidelberg 1989

Authors and Affiliations

  • V. A. Sarychev
    • 1
  • M. Yu. Belyaev
    • 1
  • V. V. Sazonov
    • 1
  • T. N. Tyan
    • 1
  1. 1.Keldysh Institute of Applied MathematicsUSSR Academy of SciencesRussia

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