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...design for cost and performance of a solid rocket motor
来自 : bhxb.buaa.edu.cn/EN/Y2005/V31/
发布时间:2021-03-24
[1] Wertz J R, Larson W J. Reducing space mission cost [M]. Torrance California:Microcosm Press, 1996[2] 杨 青,汪 亮,叶定友. 基于多目标遗传算法的固体火箭发动机面向成本优化设计[J]. 固体火箭技术, 2002,25(4):16~20 Yang Qing, Wang Liang, Ye Dingyou. Optimization design for cost of solid rocket motor based on multiobjective genetic algorithm[J]. Journal of Solid Rocket Technology, 2002,25(4):16~20(in Chinese)[3] 陈汝训主编. 固体火箭发动机设计与研究 [M]. 北京:宇航出版社,1992 Chen Ruxun. Design and research of solid rocket motor [M]. Beijing:Astronautics Press, 1992(in Chinese)[4] 张洪涛编著. 固体火箭发动机原理与设计[M]. 西安:航天科技集团公司四院,1999 Zhang Hongtao. Principle and design of solid rocket motor [M]. Xi an:The Fourth Academy of CASTC, 1999(in Chinese)[5] Huang Chunping, Zhang Wenhan, Qian Songdi. Research and application of parameter-cost model on long march series launch vehicle . IAA-96-IAA.1.1.01,USA:AIAA,1996[6] Deb K, Pratap A. A fast and elitist multiobjective genetic algorithm:NSGA-Ⅱ[J]. IEEE Transaction on Evolutionary Computation, 2002,6(2):182~197[7] Steuer E R. Multiple criteria optimization:theory, computation and application [M]. New York:John Wiley Sons Inc, 1986
rocket engines of a launch vehicle, parameter-cost models of motor parts ...Setting the maximum terminal speed increment of the rocket motor and its ...To solve the problem of multiple attributes value optimization in the ...Dual
rocket engines of a launch vehicle, parameter-cost models of motor parts ...Setting the maximum terminal speed increment of the rocket motor and its ...To solve the problem of multiple attributes value optimization in the ...Dual
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发布于 : 2021-03-24
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