Method for approximating the air-to-air missile trajectory based on the genetic algorithm

Changping Du; Deyun Zhou; Zhiping Yang

Method for approximating the air-to-air missile trajectory based on the genetic algorithm

Changping Du
, Deyun Zhou
, Zhiping Yang

电子信息学院

Northwestern Polytechnical University Xian
China Aviation Industry Corporation

科研成果: 期刊稿件 › 文章 › 同行评审

2 引用（Scopus）

摘要

A method of approximating the air to air mssile trajectory is developed based on the genetic algorithm. The approximating results have been successfully applied to the fire control design of one type of P.R.C fighter aircraft. The mathematical model of the method is described. The five steps of optimizing this mathematical model with the genetic algorithm are explained. Numerical simulation shows that this method is applicable and has a better approximating effect.

源语言	英语
页（从-至）	172-175
页数	4
期刊	Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University
卷	21
期	2
出版状态	已出版 - 4月 2003

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引用此

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abstract = "A method of approximating the air to air mssile trajectory is developed based on the genetic algorithm. The approximating results have been successfully applied to the fire control design of one type of P.R.C fighter aircraft. The mathematical model of the method is described. The five steps of optimizing this mathematical model with the genetic algorithm are explained. Numerical simulation shows that this method is applicable and has a better approximating effect.",

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AU - Zhou, Deyun

AU - Yang, Zhiping

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N2 - A method of approximating the air to air mssile trajectory is developed based on the genetic algorithm. The approximating results have been successfully applied to the fire control design of one type of P.R.C fighter aircraft. The mathematical model of the method is described. The five steps of optimizing this mathematical model with the genetic algorithm are explained. Numerical simulation shows that this method is applicable and has a better approximating effect.

AB - A method of approximating the air to air mssile trajectory is developed based on the genetic algorithm. The approximating results have been successfully applied to the fire control design of one type of P.R.C fighter aircraft. The mathematical model of the method is described. The five steps of optimizing this mathematical model with the genetic algorithm are explained. Numerical simulation shows that this method is applicable and has a better approximating effect.

KW - Air-to-air missile trajectory

KW - Approximating method

KW - Genetic algorithm

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JO - Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University

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Method for approximating the air-to-air missile trajectory based on the genetic algorithm

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