DocumentCode
3437226
Title
Notice of Retraction
Multidisciplinary design optimization based on physical programming
Author
Lei Liu ; Huanwei Xu ; Zhonglai Wang ; Hong-Zhong Huang ; Debiao Meng
Author_Institution
Sch. of Mech., Electron., & Ind. Eng., Univ. of Electron. Sci. & Technol. of China, Chengdu, China
fYear
2013
fDate
15-18 July 2013
Firstpage
555
Lastpage
558
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.
Generally, multidisciplinary design optimization (MDO) has a good performance when dealing with the coupled relationship among disciplines. However, the preference of designers could not be reflected in MDO. Therefore, some effective approaches, which can reflect preference of designers, should be proposed to handle the optimization problem with increased complexity. In this paper, an effective optimal approach is proposed based on the combination of collaborative optimization and physical programming. And then, the proposed approach is applied for the optimization of a XX-type missile. By contrast, the proposed approach has a better performance.
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.
Generally, multidisciplinary design optimization (MDO) has a good performance when dealing with the coupled relationship among disciplines. However, the preference of designers could not be reflected in MDO. Therefore, some effective approaches, which can reflect preference of designers, should be proposed to handle the optimization problem with increased complexity. In this paper, an effective optimal approach is proposed based on the combination of collaborative optimization and physical programming. And then, the proposed approach is applied for the optimization of a XX-type missile. By contrast, the proposed approach has a better performance.
Keywords
design engineering; missiles; optimisation; MDO; XX-type missile; collaborative optimization; designers; multidisciplinary design optimization; optimal approach; physical programming; Collaboration; Design optimization; Educational institutions; Missiles; Programming; Reliability engineering; MDO; collaborative optimization; optimization of missile; physical programming;
fLanguage
English
Publisher
ieee
Conference_Titel
Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE), 2013 International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4799-1014-4
Type
conf
DOI
10.1109/QR2MSE.2013.6625645
Filename
6625645
Link To Document