TY - GEN
T1 - Case-based reasoning for developing initial aircraft concepts
AU - Liu, Hu
AU - Lu, Xin Lai
AU - Luo, Ming Qiang
AU - Wu, Zhe
PY - 2006
Y1 - 2006
N2 - To make use of the knowledge and experience embedded in previous aircraft concepts, as well as improve the quality and efficiency of design by using existed information, application of case-based reasoning has been investigated. In this paper, an adapted flow of applying this technique is firstly presented according to the process of conceptual design, and the traditional methods for two tasks in this flow, i.e., case representation and retrieval, have been improved. Considering the complexity of aircraft and dynamic increase of information during conceptual design, a hierarchy model was proposed to represent a concept as aggregation of sources, groups, segments and attributes. Based on this model, a hierarchy nearest-neighbor method and a method called distance criterion for calculating group similarity were proposed to retrieve the "best-matching" case. These methods have been implemented in a design system and an example is presented to validate their effectiveness.
AB - To make use of the knowledge and experience embedded in previous aircraft concepts, as well as improve the quality and efficiency of design by using existed information, application of case-based reasoning has been investigated. In this paper, an adapted flow of applying this technique is firstly presented according to the process of conceptual design, and the traditional methods for two tasks in this flow, i.e., case representation and retrieval, have been improved. Considering the complexity of aircraft and dynamic increase of information during conceptual design, a hierarchy model was proposed to represent a concept as aggregation of sources, groups, segments and attributes. Based on this model, a hierarchy nearest-neighbor method and a method called distance criterion for calculating group similarity were proposed to retrieve the "best-matching" case. These methods have been implemented in a design system and an example is presented to validate their effectiveness.
UR - https://www.scopus.com/pages/publications/34250750333
U2 - 10.2514/6.2006-1487
DO - 10.2514/6.2006-1487
M3 - 会议稿件
AN - SCOPUS:34250750333
SN - 1563478072
SN - 9781563478079
T3 - Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
SP - 17825
EP - 17834
BT - Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 44th AIAA Aerospace Sciences Meeting 2006
Y2 - 9 January 2006 through 12 January 2006
ER -