基于模拟退火算法的自适应引战配合优化设计  

Optimized Design of Adaptive Fuze Warhead Coordination Based on Simulated Annealing Algorithm

作　　者：熊森才 祝学军[1] 刘立辉[1] 赵晓宁[1] Xiong Sencai;Zhu Xuejun;Liu Lihui;Zhao Xiaoning(China Academy of Launch Vehicle Technology,Beijing 100076,China)

机构地区：[1]中国运载火箭技术研究院,北京100076

出　　处：《战术导弹技术》2020年第3期98-104,共7页Tactical Missile Technology

基　　金：航天科技集团有限公司2017年度钱学森青年创新基金。

摘　　要：针对传统引战配合研究与制导弹药总体设计之间脱节的问题,在现有相关理论的基础上,推导了以杀爆战斗部末端姿态角、炸点位置等参数为输入,破片落点、落速为输出的引战配合模型,建立了制导弹药飞行过程与目标毁伤之间的数学关系,并将目标毁伤纳入到总体设计全流程中。实例分析计算表明,通过对弹道末端参数的优化能够有效地提高武器系统的实际毁伤效果,研究结果可为今后实现制导弹药外形结构、环境气动、制导弹道、毁伤效果一体化设计奠定良好的基础。Aiming at the problem of the traditional research of fuze-warhead coordination and the overall design of missiles,the fuze-warhead coordination model is deduced,which uses the terminal attitude angle and the explosion position of the missile as the input,the fragmentation position and the falling speed as the output. And a mathematical relationship between the missile flight process and the terminal damage is established. Then,the target damage into the overall design process is incorporated. The example analysis and calculation show that the optimization of the ballistic terminal parameters can effectively improve the actual damage effect of the weapon system,and can provide a good foundation for the integrated design of the shape structure,environmental aerodynamics,guidance-trajectory and damage effect of the guided ammunition in the future.

关 键 词：战斗部 制导弹药 引战系统 目标毁伤 破片 模拟退火算法 

分 类 号：TJ41[兵器科学与技术—火炮、自动武器与弹药工程]