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

Аннотация

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.