DocumentCode
3278826
Title
Notice of Retraction
Inertial Frame Coarse Alignment for Strapdown Inertial Navigation System
Author
Ben Yueyang ; Guisheng Yin ; Wei Gao ; Feng Sun
Author_Institution
Coll. of Comput. Sci. & Technol., Harbin Eng. Univ., Harbin, China
Volume
1
fYear
2009
fDate
15-17 May 2009
Firstpage
647
Lastpage
651
Abstract
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
The inertial frame coarse alignment is proposed to accomplish the coarse estimation of strapdown attitude matrix under the dynamic condition in which the disturbed acceleration and rotation velocity exist. This method utilizes the gravity integration on inertial frames to calculate strapdown attitude matrix, and the disturbed components could be counteracted during the integration process. The simulation results show that the proposed method is superior to the conventional one under the dynamic condition.
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
The inertial frame coarse alignment is proposed to accomplish the coarse estimation of strapdown attitude matrix under the dynamic condition in which the disturbed acceleration and rotation velocity exist. This method utilizes the gravity integration on inertial frames to calculate strapdown attitude matrix, and the disturbed components could be counteracted during the integration process. The simulation results show that the proposed method is superior to the conventional one under the dynamic condition.
Keywords
inertial navigation; transfer function matrices; inertial frame coarse alignment; strapdown attitude matrix; strapdown inertial navigation system; Acceleration; Application software; Computer science; Earth; Educational institutions; Gravity; Inertial navigation; Information technology; Vehicle dynamics; Vehicles; alignment; dynamic condition; inertial frame; strapdown attitude matrix;
fLanguage
English
Publisher
ieee
Conference_Titel
Information Technology and Applications, 2009. IFITA '09. International Forum on
Conference_Location
Chengdu
Print_ISBN
978-0-7695-3600-2
Type
conf
DOI
10.1109/IFITA.2009.463
Filename
5231727
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