Optical monitoring of inter satellite distance between Turksat-2A And Turksat-3A

Abstract

Geostationary satellites are objects, which revolve around the Earth where orbits are nearly circular and located on the equator plane with a period exactly equal to the rotation of the Earth. Most of such satellites are used for civil and military communication, television broadcasting and weather forecasting. Gravitational forces of the Sun, Moon and non-uniform mass distribution of the Earth perturb the geostationary orbits. Including these gravitational anomalies pressure of Solar winds is another source of perturbation. Because of these perturbations, orbits of geostationary satellites disturbed and some correction maneuvers must be performed. ITU radio regulation requires geostationary satellites have capability of maintaining their positions within ±0.1° of the longitude of their nominal positions [2]. Multiple numbers of colocated geostationary satellites can be operated within ±0.1° box with careful orbit determination and maneuver strategies. Most orbit determinations of the geostationary satellites are performed by tone ranging; measuring phase difference of RF signals sent to satellite and received from the satellite. Angular parameters of the satellites are obtained by azimuth and elevation of the control station antennas, which are following beacon signal of the satellite. Because of all geostationary satellites must be located on geostationary orbit, collision risk always exists. Telescope observation of geostationary satellites provides us to complimentary information to tone ranging systems, which can be used for correlation and calibration purposes.In this study, inter-satellite distances of co-located Turksat-2A and Turksat-3A satellites measured by telescope observations. This optical observation performed in 2011 at the Ankara University Observatory (AUO) using 20 cm (8-inch) optical telescope and with a CCD type detector. The inter-satellite distances are calculated by using the observed angular measurements between Turksat-2A and Turksat-3A and the radial distance measured with tone ranging. Results are compared with tone ranging orbit measurements performed by Turksat Satellite Control Center.

TrackInk: An IoT-Enabled Real-Time Object Tracking System in Space

“…The system described throughout this paper allows for a unique and flexible framework for applications in the space and sensor areas of research. Other similar systems have significantly higher cost and lack any portability [63,65]. Despite this, the described framework is able to provide a qualitative analysis of following and indicating toward satellites and celestial bodies in the sky.…”

“…In [65], the use of optical telescope observations to monitor the distance between two geosynchronous satellites, Turksat 2A and Turksat 3A, is discussed. It is discovered that an optical system is sufficient to compare the orbital paths of the two satellites and validate their simulation models.…”

Determination of Coverage Oscillation for Inclined Communication Satellite

“…GEO satellites seem to be fixed from the earth [1]. The users can have full time transmit/receive ability with a satellite by using distribution of earth, solar pressure, and electromagnetic are primary perturbing forces act on a GEO satellite [2][3][4][5]. GEO satellites have two types of movements under the external forces.…”