TY - GEN
T1 - Geosynchronous satellites orbits from optical observations
AU - Weiss, Yaniv
AU - Kaspi, Shai
AU - Shiryaev, Alexander
AU - Kogan, Alexander
AU - Behar, Ehud
N1 - Publisher Copyright:
Copyright © 2015 by the American Institute Federation of Aeronautics and Astronautics. Inc. All rights reserved.
PY - 2015/1/1
Y1 - 2015/1/1
N2 - An autonomous robotic system is developed for performing optical observations of geosynchronous (GEO) satellites, determination of their angular positions in the sky, and the improvement of their orbits. Each of the images, taken with a CCD-camera attached to the telescope, contains several exposures of the satellite together with the trails of the background stars. A new method is presented to determine the stars positions in the images, based on the rotational algorithm. The automatic processing of the CCD image taken over the night results in a number of the sequence of precise satellite angular coordinates. Using these coordinates as measurements, the orbit defined by the relevant NORAD TLE set -As a preliminary one, and an adequate dynamical model of the satellite orbital motion, an improved orbit can be obtained by the least-squares differential correction algorithm. In this way, the post-fit angular positions of AMOS-2 and -3 GEO satellites were determined with the accuracy of about 0".5 (< 100 meters). Incorporating the radar ranging measurements provides insignificant improvement to the angular position estimates.
AB - An autonomous robotic system is developed for performing optical observations of geosynchronous (GEO) satellites, determination of their angular positions in the sky, and the improvement of their orbits. Each of the images, taken with a CCD-camera attached to the telescope, contains several exposures of the satellite together with the trails of the background stars. A new method is presented to determine the stars positions in the images, based on the rotational algorithm. The automatic processing of the CCD image taken over the night results in a number of the sequence of precise satellite angular coordinates. Using these coordinates as measurements, the orbit defined by the relevant NORAD TLE set -As a preliminary one, and an adequate dynamical model of the satellite orbital motion, an improved orbit can be obtained by the least-squares differential correction algorithm. In this way, the post-fit angular positions of AMOS-2 and -3 GEO satellites were determined with the accuracy of about 0".5 (< 100 meters). Incorporating the radar ranging measurements provides insignificant improvement to the angular position estimates.
UR - http://www.scopus.com/inward/record.url?scp=84991736411&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84991736411
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 5538
EP - 5552
BT - 66th International Astronautical Congress 2015, IAC 2015
PB - International Astronautical Federation, IAF
T2 - 66th International Astronautical Congress 2015: Space - The Gateway for Mankind's Future, IAC 2015
Y2 - 12 October 2015 through 16 October 2015
ER -