DocumentCode
2688605
Title
Notice of Retraction
Attitude solution of vertical penetrative trajectory based on quaternion
Author
Da-wei Liu ; Qun-li Xia ; Qiu-qiu Wen
Author_Institution
Dept. of Flying Vehicle Design, Beijing Inst. of Technol., Beijing, China
Volume
1
fYear
2010
fDate
24-26 Aug. 2010
Firstpage
293
Lastpage
296
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.
In vertical penetrative trajectory, attitude solution will be singularity when pitch angle is -90deg, this paper take attention to study an omnidirectional space attitude solution method of vertical penetrative trajectory base on quaternion. Firstly, relations between quaternion transformation matrix and Euler angle transformation matrix are analyzed, then, omnidirectional space quaternion initialization method, quaternion update arithmetic and the method of Euler angles account from quaternion are studied. Secondly, the vertical penetrative trajectory simulation model based on quaternion is established to resolve the singularity problem of attitude solution in vertical penetrative trajectory based on Euler angle, the accurate omnidirectional space attitude solution is obtained. Finally, a series of vertical penetrative trajectory simulations demonstrate that the method is perfectly feasible and convince to be used in the attitude solution of vertical penetrative trajectory engineering design.
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.
In vertical penetrative trajectory, attitude solution will be singularity when pitch angle is -90deg, this paper take attention to study an omnidirectional space attitude solution method of vertical penetrative trajectory base on quaternion. Firstly, relations between quaternion transformation matrix and Euler angle transformation matrix are analyzed, then, omnidirectional space quaternion initialization method, quaternion update arithmetic and the method of Euler angles account from quaternion are studied. Secondly, the vertical penetrative trajectory simulation model based on quaternion is established to resolve the singularity problem of attitude solution in vertical penetrative trajectory based on Euler angle, the accurate omnidirectional space attitude solution is obtained. Finally, a series of vertical penetrative trajectory simulations demonstrate that the method is perfectly feasible and convince to be used in the attitude solution of vertical penetrative trajectory engineering design.
Keywords
arithmetic; attitude control; matrix algebra; missile guidance; Euler angle transformation matrix; omnidirectional space attitude solution method; omnidirectional space quaternion initialization method; quaternion transformation matrix; quaternion update arithmetic; singularity problem; vertical penetrative trajectory simulation model; Quaternions; Euler angle; attitude solution; quaternion; vertical penetrative trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer, Mechatronics, Control and Electronic Engineering (CMCE), 2010 International Conference on
Conference_Location
Changchun
Print_ISBN
978-1-4244-7957-3
Type
conf
DOI
10.1109/CMCE.2010.5610494
Filename
5610494
Link To Document