DocumentCode
2870850
Title
Study on Attitude Algorithm for Initial Alignment of SINS on Dynamic base
Author
Zhao, Lin ; Nie, Qi ; Xia, Linlin
Author_Institution
Coll. of Autom., Harbin Eng. Univ.
fYear
2006
fDate
25-28 June 2006
Firstpage
2247
Lastpage
2252
Abstract
In this paper, an improved attitude algorithm of SINS´s alignment is presented due to the disturbances of the ships under wind and wave. The author proposes the attitude algorithm module of alignment on dynamic base and analyzes sufficiently the function of the algorithm. The scheme experiences a series of tests on three-axis turning table on validity of the simulation results. In sequence sea test was carried out in Yellow Sea. According to the experiment data, attitude error curves in alignment are also clearly given using quaternion algorithms. The test results show that this presented algorithm can realize fast alignment and high precision in SINS self-alignment
Keywords
attitude control; inertial navigation; position control; ships; velocity control; SINS self-alignment; attitude algorithm; attitude error curves; ships; strapdown inertial navigation system; three-axis turning table; Algorithm design and analysis; Angular velocity; Automation; Inertial navigation; Marine vehicles; Quaternions; Silicon compounds; Software testing; System testing; Turning; Simulation; Test on three-axis turning table; alignment on dynamic base; initial alignment; quaternion algorithm; sea test; strapdown inertial navigation system (SINS);
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation, Proceedings of the 2006 IEEE International Conference on
Conference_Location
Luoyang, Henan
Print_ISBN
1-4244-0465-7
Electronic_ISBN
1-4244-0466-5
Type
conf
DOI
10.1109/ICMA.2006.257661
Filename
4026447
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