TY - GEN
T1 - Probability and integration judgment based best selection of aircraft conceptual/preliminary scheme
AU - Sun, Kang Wen
AU - Huang, Jun
PY - 2013
Y1 - 2013
N2 - The technical feasibility analysis of an aircraft design scheme directly influences the design proposal, which determines whether scheme can satisfy the maximum design requirements or we can continue the detailed design. Conventional design evaluation of a new technical influence is insufficient, because the weight evaluation (analytic hierarchy process, AHP) is usually subjective. This paper proposes a new impact analysis method based on probability theory, and the comprehensive information including the data envelopment analysis (DEA) and the interval number AHP is referred to as a comprehensive empowerment of the appraisal criterion. According to the proposed method, the best selection method of an aircraft conceptual/preliminary scheme based on probability and integration judgment is established. Finally, some examples are presented to demonstrate the validity of the method.
AB - The technical feasibility analysis of an aircraft design scheme directly influences the design proposal, which determines whether scheme can satisfy the maximum design requirements or we can continue the detailed design. Conventional design evaluation of a new technical influence is insufficient, because the weight evaluation (analytic hierarchy process, AHP) is usually subjective. This paper proposes a new impact analysis method based on probability theory, and the comprehensive information including the data envelopment analysis (DEA) and the interval number AHP is referred to as a comprehensive empowerment of the appraisal criterion. According to the proposed method, the best selection method of an aircraft conceptual/preliminary scheme based on probability and integration judgment is established. Finally, some examples are presented to demonstrate the validity of the method.
KW - Best selection
KW - Integration judgment
KW - Probability
KW - The technical feasibility of aircraft design scheme
UR - https://www.scopus.com/pages/publications/84891551536
U2 - 10.1007/978-3-642-33012-4_65
DO - 10.1007/978-3-642-33012-4_65
M3 - 会议稿件
AN - SCOPUS:84891551536
SN - 9783642330117
T3 - Proceedings of 2012 3rd International Asia Conference on Industrial Engineering and Management Innovation, IEMI 2012
SP - 655
EP - 664
BT - Proceedings of 2012 3rd International Asia Conference on Industrial Engineering and Management Innovation, IEMI 2012
PB - Springer Science and Business Media Deutschland GmbH
T2 - 2012 3rd International Asia Conference on Industrial Engineering and Management Innovation, IEMI 2012
Y2 - 10 August 2012 through 11 August 2012
ER -