DocumentCode
14714
Title
Optimal attitude and position determination by integration of INS, star tracker, and horizon sensor
Author
Rad, Amir Moghtadaei ; Nobari, Jafar Heyrani ; Nikkhah, Amir Ali
Author_Institution
Dept. of Electr. Eng., Islamic Azad Univ., Tehran, Iran
Volume
29
Issue
4
fYear
2014
fDate
Apr-14
Firstpage
20
Lastpage
33
Abstract
Navigation, for many years, has been one of the issues that preoccupied the human mind. The compass was the first instrument built for navigation by the Chinese. The compass determined geographical north instead of a magnetic one [1]. Gradually over time, humans found that it was possible to make orientations by celestial bodies. However, positioning was still impossible. In 1757, the first sextant able to measure angles of celestial bodies and the Earth´s horizon was invented by John Bird [1], [2], [3]. Also, the first star catalog containing 992 stars was obtained by Hip-parchus in 1437. The star catalog and the sextant were used for simple navigation [4]. More elaborate star catalogs were developed by advanced sky observation devices, such as SKY2000 with 299,460 stars, introduced in 2006 [5].
Keywords
attitude measurement; compasses; inertial navigation; star trackers; INS; horizon sensor; optimal attitude; position determination; sextant; star catalog; star tracker; Aircraft navigation; Attitude control; Intertial navigation; Navigation; Position measurement; Remote sensing; Terrestrial atmosphere; Unified modeling language;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems Magazine, IEEE
Publisher
ieee
ISSN
0885-8985
Type
jour
DOI
10.1109/MAES.2014.130093
Filename
6819121
Link To Document