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...design for cost and performance of a solid rocket motor
来自 : bhxb.buaa.edu.cn/EN/abstract/a 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

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发布于 : 2021-03-24 阅读(0)
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