| 导弹总体设计参数优选的一种技术 |
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| 引用本文： | 刘宗映 金良超. 导弹总体设计参数优选的一种技术[J]. 宇航学报, 1989, 0(2): 1-9 |
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| 作者姓名： | 刘宗映 金良超 |
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| 作者单位： | 上海航天局805所(刘宗映)，航天工业部708所(金良超) |
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| 摘 要： | 本文讨论导弹总体设计参数的优选问题。通过实例,讨论了正交设计和逐次撒网登高相结合的优选方法的应用。结果表明,本文提供的方法计算量小,效率高,简便实用。
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| 关 键 词： | 导弹 总体设计 参数优选 |
A TECHNIQUE ON OPTIMAL SELECTION OF THE GENERAL DESIGN PARAMETERS OF THE MISSILE |
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| Liu Zhongying Jin Liangchao. A TECHNIQUE ON OPTIMAL SELECTION OF THE GENERAL DESIGN PARAMETERS OF THE MISSILE[J]. Journal of Astronautics, 1989, 0(2): 1-9 |
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| Authors: | Liu Zhongying Jin Liangchao |
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| Affiliation: | Liu Zhongying Jin Liangchao |
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| Abstract: | This paper discusses a Technique on optimal selection problem of the general design parameters of the missile. In this papaer, an example is given to illustrate the application of the optimal selection technique on combining the orthogonal design with step-by-step casting net and mounting high. The results show that a small amount of calculation, high efficincy and more convenient to use are the advantages of this technique. |
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| Keywords: | General design of the missile Optimal selection of the parameten Orthogonal design. Method of step-by-step casting net and mounting high. |
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