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Generation of satellite tracking profile: Problems and validation algorithms

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Abstract
Recently, as a satellite mission becomes complicated, it has been required to generate the schedule of satellite antenna movements automatically without relying upon operator's ad hoc knowledge. To generate the satellite antenna schedule autonomously, this paper first addresses geometrical problems associated with the antenna scheduling and mission planning problems that can be formulated from satellite navigation and antenna orientation information. Then, based on the solutions of the geometrical problems, a set of antenna azimuth and elevation angles that enables the antenna to point towards the desired ground station is obtained systematically. Using the computed azimuth and elevation angles, the satellite tracking profile (TP) is generated, and to validate it, TP validation algorithms are developed. (C) 2014 COSPAR. Published by Elsevier Ltd. All rights reserved.
Author(s)
Lee, Jae-GyeongAhn, Hyo-SungKo, Kwang-HeeWang, SemyungJung, Ok-ChulChoi, Su-JinChung, Daewon
Issued Date
2014-09
Type
Article
DOI
10.1016/j.asr.2014.05.021
URI
https://scholar.gist.ac.kr/handle/local/15037
Publisher
ELSEVIER SCI LTD
Citation
Advances in Space Research, v.54, no.6, pp.1092 - 1107
ISSN
0273-1177
Appears in Collections:
Department of Mechanical and Robotics Engineering > 1. Journal Articles
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