DocumentCode :
1873011
Title :
A study on the TFN-based AHP model for the evaluation of missile systems performance
Author :
Cao, Jian ; Yang, Chunjie ; Yang, Yan
Author_Institution :
Inst. of Inf. Intelligence & Decision Optimization, Zhejiang Univ. of Technol., Hangzhou
fYear :
2006
fDate :
19-21 Jan. 2006
Lastpage :
529
Abstract :
To reduce the complexity of evaluating missile systems performance, a new fuzzy AHP model based on the analytic hierarchy process (AHP) and basic theory of the trigonometrical fuzzy number (TFN) was given and corresponding evaluation process was introduced. In Matlab environment an illustrative example was presented and analyzed. The results indicate that applying TFN and LLSM to AHP makes the model combine subjective analysis with quantitative analysis effectively, synthesize group opinions adequately, and acquire the consistent degree of decisions under each criterion from different experts clearly. In addition, the model can be operated by programming easily and applied widely due to its simple, normative arithmetic formulas
Keywords :
fuzzy set theory; missile guidance; Matlab; analytic hierarchy process; arithmetic formulas; logarithmic least square method; missile systems; trigonometrical fuzzy number; Decision making; Fuzzy control; Fuzzy systems; Humans; Least squares methods; Mathematical model; Missiles; Performance analysis; System performance; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems and Control in Aerospace and Astronautics, 2006. ISSCAA 2006. 1st International Symposium on
Conference_Location :
Harbin
Print_ISBN :
0-7803-9395-3
Type :
conf
DOI :
10.1109/ISSCAA.2006.1627678
Filename :
1627678
Link To Document :
بازگشت