TY - JOUR
T1 - Improved method of BLISS based on response surface
AU - Zhang, Dai Yu
AU - Song, Bao Wei
AU - Wang, Peng
AU - Dong, Hua Chao
PY - 2013/8
Y1 - 2013/8
N2 - Based on the analysis of the BLISS (bi-level integrated system synthesis), an improved method of BLISS was proposed, and the response surface based on design of experiments was introduced to make an approximation in both the subsystem and the system-level meanwhile the parameters of moving step were set, making unnecessary for complex sensitivity analysis; the movement limits of each iterative optimization in the BLISS method, and the optimization iterations and the possibility of falling into local optimum were reduced. Finally, two specific examples were given to verify above method compared with traditional BLISS. The results show that the optimization iterations of above methods were respectively reduced by 57.9% and 70.3%, respectively.
AB - Based on the analysis of the BLISS (bi-level integrated system synthesis), an improved method of BLISS was proposed, and the response surface based on design of experiments was introduced to make an approximation in both the subsystem and the system-level meanwhile the parameters of moving step were set, making unnecessary for complex sensitivity analysis; the movement limits of each iterative optimization in the BLISS method, and the optimization iterations and the possibility of falling into local optimum were reduced. Finally, two specific examples were given to verify above method compared with traditional BLISS. The results show that the optimization iterations of above methods were respectively reduced by 57.9% and 70.3%, respectively.
KW - Bi-level integrated system synthesis
KW - Design of experiments
KW - Multidisciplinary design optimization (MDO)
KW - Response surface
KW - Sensitivity analysis
UR - http://www.scopus.com/inward/record.url?scp=84882952708&partnerID=8YFLogxK
M3 - 文章
AN - SCOPUS:84882952708
SN - 1000-8055
VL - 28
SP - 1797
EP - 1802
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 8
ER -