基于Agent建模的机载激光武器系统作战效能影响因素分析

doi:10.3969/j.issn.1001-506X.2020.04.13

摘要/Abstract

摘要：

为了研究机载激光武器的安装对轰炸机作战效能的影响，提出了基于功能组件的模块化作战仿真框架。采用基于Agent的建模与仿真方法,基于感知、通信、决策、运动、执行的功能对Agent模块进行划分,提出了基于功能组件的模块化作战仿真体系。在此模型框架下,设计机载激光武器系统、雷达系统、导弹等模块的状态机,并建立考虑相对位置变化的详细数学模型,以分析在战斗每一时刻影响作战效能的指标参数变化情况。最后通过对典型突防作战算例的仿真,研究了在动态作战过程中激光武器的发射镜直径和发射功率与目标表面光斑大小和能量密度随相对距离的变化关系,分析了在载机为高速小雷达散射截面积(radar cross section, RCS)和低速大RCS两种情况下,机载激光武器的发射镜直径和发射功率对轰炸机突防效能的影响。分析结果表明,提高机载激光武器的发射功率和发射镜直径对作战效能提升显著,尤其是在载机为低速大RCS的情况下对效能的提升非常显著。

关键词: 机载激光武器, Agent, 作战仿真, 作战效能

Abstract:

To study the influence of airborne laser weapon system to bomber mission effectiveness, a capability based on the modularized simulation system is proposed. An Agent-based modeling and simulation method is used. A capability based modularized simulation system is proposed based on five agent capabilities: sensing, communication, decision, movement and execution. The state machines of airborne laser weapon system, radar system and missile system are designed within this structure. In order to analyze the dynamic change of combat effectiveness, the mathematical models proposed are related to target positions. Then, a simulation of typical penetration operation is conducted to analyze the influence of mirror diameter and initial power of airborne laser weapon system. Finally, the influence of aircraft capability on airborne laser weapon system is analyzed through a simulation with low-speed low-radar cross section (RCS) aircraft and high-speed high-RCS aircraft. The results show that increasing the mirror diameter and initial power of airborne laser weapons can increase the combat effectiveness significantly, especially to low-speed RCS aircraft.

Key words: airborne laser, Agent, combat simulation, combat effectiveness

中图分类号:

V271.4

郧奇佳, 宋笔锋, 裴扬, 王冠坤. 基于Agent建模的机载激光武器系统作战效能影响因素分析[J]. 系统工程与电子技术, 2020, 42(4): 826-835.

Qijia YUN, Bifeng SONG, Yang PEI, Guankun WANG. Analysis of the factors influencing the combat effectiveness of airborne laser weapon system based on Agent modeling[J]. Systems Engineering and Electronics, 2020, 42(4): 826-835.

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Agent	参数	数值
飞机	突防速度Ma_a/Ma	1.5
	突防高度H_a/km	10
	RCS σ_t/m²	0.1
	探测传感器焦距f/mm	20
	粗跟踪焦距f/mm	100
	精跟踪焦距f/mm	400
	焦平面阵列分辨率r_FPA/μm	1
	光束质量因子β	2
	激光波长λ/μm	1.06
	激光聚焦距离R/km	2~30
环境	大气能见度V_M/km	20
	大气密度kg/m³	1.29
	大气比热容c_p/(J/kg·K)	1 005
	大气折射率随温度变化率n_T	10^-6
	气溶胶类型常数K	4.543
舰船	航行速度/节	20
	雷达特征探测RCS σ₀/m²	5
	雷达特征探测概率P_d0	0.9
	雷达特征探测距离R₀/km	100
	雷达特征虚警概率P_FA0	10^-6
	恒虚警处理参考单元数N	16
	雷达搜索循环时间T_s/s	5
	雷达跟踪循环时间T_t/s	0.1
导弹	导弹尺寸/m	0.5×0.5×2
	飞行速度Ma_m/Ma	3
	导引头作用距离R_d/km	10
	导引头材料对激光的吸收率	0.7
	毁伤阈值E_d/(kJ/cm²)	1

指标	最小值	最大值	步长	实验点
P/kW	50	250	10	21
D/m	0.3	0.7	0.1	5
总实验点数				105

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