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遗传算法解算弹道导弹再入弹道
引用本文:范锐锐,王明海. 遗传算法解算弹道导弹再入弹道[J]. 弹箭与制导学报, 2010, 30(5)
作者姓名:范锐锐  王明海
作者单位:第二炮兵工程学院,西安,710025
摘    要:基于弹道导弹再入段运动数学模型,提出了预定程序弹道再入突防的方法并进行了遗传算法解算突防弹道的研究。建立了以攻角随再入时间增长的变化量为编码对象的遗传算法模型并进行仿真计算。仿真结果表明,该算法能够实现预定程序再入弹道快速高精度的解算,具有工程的应用价值。

关 键 词:弹道导弹  再入弹道  遗传算法  

Solution of Reentry Trajectory of Ballistic Missile Using Genetic Algorithm
FAN Ruirui,WANG Minghai. Solution of Reentry Trajectory of Ballistic Missile Using Genetic Algorithm[J]. Journal of Projectiles Rockets Missiles and Guidance, 2010, 30(5)
Authors:FAN Ruirui  WANG Minghai
Affiliation:FAN Ruirui,WANG Minghai (The Second Artillery Engineering College,Xi'an 710025,China)
Abstract:Based on the mathematic model of reentry movement of ballistic missile,the method of adopting preprogram trajectory to penetrate was established and solution of the penetration trajectory using genetic algorithm was studied.The genetic algorithm model which took the angle of attack changing along with reentry time increasing as the object of coding was introduced and the simulation was continued.The simulation result shows genetic algorithm can carry out the accuracy result of reentry trajectory solution wi...
Keywords:ballistic missile  reentry trajectory  genetic algorithm  
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