Email this article Effect of angular aberration using the example of the laser location of a spacecraft in a geosynchronous orbit
- Authors: Zinacheva T.S.1, Denisov M.M.1
-
Affiliations:
- Moscow Aviation Institute
- Issue: Vol 81, No 1 (2017)
- Pages: 18-21
- Section: Proceedings of the XV National Sukhorukov Seminar “Wave Phenomena in Inhomogeneous Media” (Waves 2016)
- URL: https://journals.rcsi.science/1062-8738/article/view/184922
- DOI: https://doi.org/10.3103/S1062873817010300
- ID: 184922
Cite item
Open Access
Access granted
Subscription Access
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.
About the authors
T. S. Zinacheva
Moscow Aviation Institute
Author for correspondence.
Email: zino4K@bk.ru
Russian Federation, Moscow, 117405
M. M. Denisov
Moscow Aviation Institute
Email: zino4K@bk.ru
Russian Federation, Moscow, 117405
Supplementary files
