DocumentCode
3513109
Title
Compensation Algorithm of Device Error for Rate Strapdown Inertial Navigation System
Author
Wang, Jie ; Gu, Hongqiang
Author_Institution
Sch. of Mech. Eng., Shijiazhuang
fYear
2008
fDate
1-3 Nov. 2008
Firstpage
667
Lastpage
670
Abstract
Based on the character of Strapdown Inertial Navigation System (SINS) on certain ballistic missile, using established mathematical model of inertial measuring system, the compensation method of SINS between samplings is deduced, which supply reference in the design of software compensation algorithm. The experiment result shows that, after using the software designed by the Algorithm, the error of IMU is reduced and the SINS accuracy is improved effectively.
Keywords
ballistics; inertial navigation; military computing; missiles; software engineering; ballistic missile; compensation algorithm; inertial measuring system; rate strapdown inertial navigation system; software compensation algorithm; Accelerometers; Angular velocity; Gyroscopes; Inertial navigation; Intelligent networks; Missiles; Pulse measurements; Sampling methods; Silicon compounds; Software algorithms; SINS; compensation algorithm; device error;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Networks and Intelligent Systems, 2008. ICINIS '08. First International Conference on
Conference_Location
Wuhan
Print_ISBN
978-0-7695-3391-9
Electronic_ISBN
978-0-7695-3391-9
Type
conf
DOI
10.1109/ICINIS.2008.137
Filename
4683314
Link To Document