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Effect of angular aberration using the example of the laser location of a spacecraft in a geosynchronous orbit

  • Proceedings of the XV National Sukhorukov Seminar “Wave Phenomena in Inhomogeneous Media” (Waves 2016)
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Bulletin of the Russian Academy of Sciences: Physics Aims and scope

Abstract

A mathematical model for the laser location of a spacecraft in a geosynchronized orbit is generated in a rotating reference system. A formula for calculating the angular aberration that appears when the noninertial reference system is considered is derived. The maximum and minimum values of angular aberration are calculated for when the laser station is at the Equator.

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Authors and Affiliations

  1. Moscow Aviation Institute, National Research University, Moscow, 117405, Russia

    T. S. Zinacheva & M. M. Denisov

Authors
  1. T. S. Zinacheva
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  2. M. M. Denisov
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Corresponding author

Correspondence to T. S. Zinacheva.

Additional information

Original Russian Text © T.S. Zinacheva, M.M. Denisov, 2017, published in Izvestiya Rossiiskoi Akademii Nauk, Seriya Fizicheskaya, 2017, Vol. 81, No. 1, pp. 25–28.

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Zinacheva, T.S., Denisov, M.M. Effect of angular aberration using the example of the laser location of a spacecraft in a geosynchronous orbit. Bull. Russ. Acad. Sci. Phys. 81, 18–21 (2017). https://doi.org/10.3103/S1062873817010300

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  • DOI: https://doi.org/10.3103/S1062873817010300

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