DocumentCode :
3405207
Title :
The star sensor layout based on geometric position analysis
Author :
Zhao, Lin ; Su, Zhonghua ; Hao, Yong
Author_Institution :
Coll. of Autom., Harbin Eng. Univ., Harbin, China
fYear :
2012
fDate :
15-17 Aug. 2012
Firstpage :
141
Lastpage :
144
Abstract :
Aiming at solving the problem that the measurement accuracy and veracity of the star sensor is seriously affected by stray light for a geocentric pointing three-axis stabilized satellite, this paper analyzed how the sunlight and the moonlight impacted on the star sensor during the satellite on-orbit running. This method is proposed on basic of studying geometric position of Sun, Earth, Moon and the satellite, considering several elements including the satellite attitude, the star-sensor installation location and field of vision(FOV). Moreover, according to the layout of star-sensor, recommended plans at different time are discussed and given, which can avoid bad influences of stray light effectively.
Keywords :
aerospace instrumentation; star trackers; stray light; Earth geometric position analysis; Moon geometric position analysis; geocentric pointing three-axis stabilized satellite; moonlight impact; satellite attitude; satellite on-orbit running; solar geometric position analysis; star sensor veracity; star-sensor field-of-vision; star-sensor installation location; stray light; sunlight impact; Earth; Extraterrestrial measurements; Moon; Optical sensors; Orbits; Vectors; geometric position; layout; star sensor;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Automation and Logistics (ICAL), 2012 IEEE International Conference on
Conference_Location :
Zhengzhou
ISSN :
2161-8151
Print_ISBN :
978-1-4673-0362-0
Electronic_ISBN :
2161-8151
Type :
conf
DOI :
10.1109/ICAL.2012.6308186
Filename :
6308186
Link To Document :
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