DocumentCode :
2553918
Title :
Application of two methods for alignment of FOG INS
Author :
Wang, Jinxi ; Lu, Wen ; Li, Lanfei
Author_Institution :
Dept. of Radiol., Taishan Med. Coll., Tai´´an, China
fYear :
2010
fDate :
16-18 April 2010
Firstpage :
581
Lastpage :
584
Abstract :
Initial alignment is of vital importance to inertial navigation systems (INS). There are mailnly two popular methods in self-alignment, which are traditional gyrocompassing alignment algorithm and kalman filter algorithm. After giving the basic principle of the two, we do some simulation and test in use of INS based fiber opitic gyroscope (FOG). The simulation and real experiment show that kalman filter is better than gyrocompassing in level alignment, however, the accuracy of azimuth misalignment angle estimation is lower. The real data test result is as similar as simulation. This provides a useful reference for design alignment algorithm for FOG INS.
Keywords :
Kalman filters; fibre optic gyroscopes; inertial navigation; FOG INS; Kalman filter algorithm; fiber optic gyroscope; gyrocompassing alignment algorithm; inertial navigation systems; initial alignment; Accelerometers; Azimuth; Earth; Field programmable gate arrays; Filters; Gyroscopes; Navigation; Silicon compounds; Space technology; Testing; FOG INS; gyrocompassing; initial alignment; kalman filter;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Information Management and Engineering (ICIME), 2010 The 2nd IEEE International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4244-5263-7
Electronic_ISBN :
978-1-4244-5265-1
Type :
conf
DOI :
10.1109/ICIME.2010.5478076
Filename :
5478076
Link To Document :
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