DocumentCode
533216
Title
Notice of Retraction
The character inversion of the mid-course missile based on the sphere-ellipse model
Author
Ding Xiao-Feng ; Zhang Yue-Hui ; Wei Xi-Zhang ; Li Yong
Author_Institution
Sch. of Electron. Sci. & Eng., Nat. Univ. of Defense Technol., Changsha, China
Volume
11
fYear
2010
fDate
22-24 Oct. 2010
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.
This paper is for the identification from the RCS sequence of the mid-course missile. On the base of analyzing its motion and electromagnetic scattering characteristic, a new method using RCS magnitude changes with respect to the object gesture angle for extracting the mid-course object´s two-dimensional length is presented. Comparing with the traditional method, the new method overcomes the disadvantage of the necessity for the maximal and minimal RCS value of the object. The experiment results tested by the simulated and anechoic chamber data of the representative missile object show the effectiveness of the method.
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.
This paper is for the identification from the RCS sequence of the mid-course missile. On the base of analyzing its motion and electromagnetic scattering characteristic, a new method using RCS magnitude changes with respect to the object gesture angle for extracting the mid-course object´s two-dimensional length is presented. Comparing with the traditional method, the new method overcomes the disadvantage of the necessity for the maximal and minimal RCS value of the object. The experiment results tested by the simulated and anechoic chamber data of the representative missile object show the effectiveness of the method.
Keywords
anechoic chambers (electromagnetic); electromagnetic wave scattering; missiles; radar cross-sections; RCS sequence; anechoic chamber data; character inversion; electromagnetic scattering; mid-course missile; object gesture angle; radar cross section; simulated chamber data; sphere-ellipse model; two-dimensional length; Anechoic chambers; Data models; Estimation; Missiles; Radar cross section; Solid modeling; Ellipse model; Inversion; Mid-course missile; Radar Cross Section;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Application and System Modeling (ICCASM), 2010 International Conference on
Conference_Location
Taiyuan
Print_ISBN
978-1-4244-7235-2
Type
conf
DOI
10.1109/ICCASM.2010.5623197
Filename
5623197
Link To Document