| 导弹自控终点散布与发射初始姿态关系建模研究 |
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| 引用本文： | 赵国荣,赵修平,戴绍武,郭晓军.导弹自控终点散布与发射初始姿态关系建模研究[J].系统仿真学报,2001(Z2). |
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| 作者姓名： | 赵国荣 赵修平 戴绍武 郭晓军 |
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| 作者单位： | 海军航空工程学院 山东烟台264001
(赵国荣，赵修平，戴绍武)，海军航空工程学院 山东烟台264001(郭晓军) |
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| 摘 要： | 在给定导弹自控终点纵向散布的情况下,如何界定导弹的发射初始姿态域?是动基座发射的导弹武器系统必须面对的问题,它对确定导弹武器系统战术技术指标、发射方式和战斗使用等至关重要。文章通过设计正交试验表、弹道仿真和回归分析等技术途径,建立了导弹自控终点纵向散布和初始发射姿态之间的数学模型,依据此模型并给定导弹自控终点纵向散布,采用非线性规划方法,可获得初始姿态域。
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| 关 键 词： | 导弹自控终点纵向散布 初始姿态域 正交试验 建模 非线性规划 |
Modeling Between a Scatter of Terminal Point of Self-control Phase of a Missile and Intervals of Initial Altitude |
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| ZHAO Guo-rong,ZHAO Xiu-ping,DAI Shao-wu,GUO Xiao-jun.Modeling Between a Scatter of Terminal Point of Self-control Phase of a Missile and Intervals of Initial Altitude[J].Journal of System Simulation,2001(Z2). |
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| Authors: | ZHAO Guo-rong ZHAO Xiu-ping DAI Shao-wu GUO Xiao-jun |
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| Abstract: | By a known longitudinal scatter of terminal point of self-control phase of a missile, how to find out its intervals of initial altitude that is necessary to definite tactical and technical index, launch mode, combat use, is an inevitable problem to weapon system of a missile based on moving launch plate. In this paper, by design of orthogonal experiment, ballistic simulation, regression analysis, a mathematical model is obtained between a scatter of terminal point of self-control phase of a missile and intervals of initial altitude. Based on this model and a known longitudinal scatter, by nonlinear programming method, intervals of initial altitude can be obtained. |
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| Keywords: | scatter of terminal point of self-control phase of a missile intervals of initial altitude orthogonal experiment modeling nonlinear programming |
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