DocumentCode :
2201913
Title :
Research of Strapdown Inertial Navigation System monitor technique based on dual-axis consequential rotation
Author :
Cheng Jianhua ; Li, Chen ; Chen Daidai ; Chen Li ; Shi Junyu
Author_Institution :
Coll. of Autom., Harbin, China
fYear :
2011
fDate :
6-8 June 2011
Firstpage :
203
Lastpage :
208
Abstract :
According to the accumulation characteristic of SINS positioning error caused by inertial sensor error, this paper brought the rotation monitor technique to improve the SINS accuracy. Dual-axis consequential rotation scheme is designed by deeply analyze toward the existing single-axis and two-axis scheme. This scheme is selected as the final scheme by analyzing modulation results of constant gyro drift, the gyro scale error and the deviation of the gyro installation error. Computer simulation shows that this scheme has better modulation than single-axis and two-axis continuous scheme and can improve position accuracy of SINS effectively.
Keywords :
error analysis; fibre optic gyroscopes; inertial navigation; inertial systems; SINS; constant gyro drift; dual-axis consequential rotation; gyro installation error; gyro scale error; inertial sensor error; positioning error; rotation monitor technique; strapdown inertial navigation system; Accuracy; Clocks; Inertial navigation; Modulation; Monitoring; Silicon compounds; Error Analyze; Rotation Modulation; Strapdown Inertial Navigation System; sensor error;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Information and Automation (ICIA), 2011 IEEE International Conference on
Conference_Location :
Shenzhen
Print_ISBN :
978-1-4577-0268-6
Electronic_ISBN :
978-1-4577-0269-3
Type :
conf
DOI :
10.1109/ICINFA.2011.5948988
Filename :
5948988
Link To Document :
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