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 :
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