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推进剂剩余量的均匀设计建模
引用本文:金宏,安维廉. 推进剂剩余量的均匀设计建模[J]. 导弹与航天运载技术, 1994, 0(6)
作者姓名:金宏  安维廉
作者单位:北京飞龙公司
摘    要:本文主要运用均匀设计[1]的均匀分散布点方法,设计了模拟推进剂剩余量的试验方案,建立了推进剂剩余量的线性模型,并与传统的模拟打靶试验相比较,取得良好效果。均匀设计的最大优点是,以很少的试验次数,获取一般规律性的东西,这对战略导弹的研制、试验、评定具有很好的使用价值。

关 键 词:~+均匀设计,推进剂余量,数学模型

Uniform Design Modeling of Propellant Remainder
Jin Hong,An Weilian. Uniform Design Modeling of Propellant Remainder[J]. Missiles and Space Vehicles, 1994, 0(6)
Authors:Jin Hong  An Weilian
Affiliation:Beijing Fei Long Company
Abstract:By using uniform design's arraying experimental points,an experimental plan which simulates the amount of propellant remainder is given,a linear model about the amount of propellant remainder is built up and a good result is achieved comparing with usual simulating target experiments.The greatest characteristic of the uniform design is that a general regularity can be obtained through few experiments and this is useful to development,test and assessment of strategic missile.
Keywords:?Uniform design   Remaining propellant mass  Mathematical model.
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