DocumentCode
1797639
Title
Geomagnetic field aided inertial navigation using the SITAN algorithm
Author
Zhiguo Dai ; Chong Kang
Author_Institution
Coll. of Sci., Harbin Eng. Univ., Harbin, China
fYear
2014
fDate
15-17 Nov. 2014
Firstpage
79
Lastpage
83
Abstract
The SITAN algorithm makes use of terrain elevation information to aid inertial navigation system and achieves good results. The geomagnetic field can be used as the conditions of the auxiliary inertial navigation, because the geomagnetic value map and the terrain elevation map have high similarity. By using the SITAN algorithm and combining the contour information of existed geomagnetic map with the processed by the method of interpolation and linear processing at the same time, the aid inertial navigation simulation was carried out for the measured geomagnetic map to provide reference for a new passive and covert method of geomagnetic field aided navigation.
Keywords
aerospace computing; aircraft navigation; geomagnetic navigation; inertial navigation; interpolation; terrain mapping; SITAN algorithm; Sandia inertial terrain aided navigation algorithm; geomagnetic field aided inertial navigation; geomagnetic value map; interpolation method; linear processing method; terrain elevation information; terrain elevation map; Equations; Inertial navigation; Kalman filters; Linearization techniques; Mathematical model; Noise; Aided Inertial Navigation; Geomagnetic field; Linearization technique; SITAN algorithm; Terrain elevation;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Informatics (ICSAI), 2014 2nd International Conference on
Conference_Location
Shanghai
Print_ISBN
978-1-4799-5457-5
Type
conf
DOI
10.1109/ICSAI.2014.7009263
Filename
7009263
Link To Document