摘要
在当前日益复杂的作战环境下,有必要对高新技术导弹武器系统进行攻防对抗研究。针对攻防对抗这一复杂的动态过程,建立了高超声速巡航导弹攻防对抗仿真体系,并在此体系框架下,分别给出了作战环境模型、结果评判模型和进攻方与防御方的交战仿真模型。根据所建立的数学模型,计算出高超声速巡航导弹的突防概率与毁伤概率,最后得到高超声速巡航导弹的作战效能。仿真结果表明,减小高超声速巡航导弹的雷达反射截面积(RCS)和增大高超声速巡航导弹的巡航速度是提高其突防效能和作战效能的重要手段。
During current complex combat conditions, investigation of combat engagement of a new technology missile weapon" system is necessary. Aimed at the complex dynamic course of combat engagement, a framework for hypersonic cruise missile combat engagement simulation is established. The combat engagement models of offensive side and defensive side are established in this framework, as well as combat environment models and estimation models. Using these models, penetration probability and damage probability of the hypersonic cruise missile are computed. Finally, combat effectiveness of the hypersonic cruise missile is given. The results show that reducing the RCS and increasing the cruise velocity of the hypersonic cruise missile are two important approaches to improve the penetration effectiveness and combat effectiveness.
出处
《飞行力学》
CSCD
北大核心
2007年第3期92-96,共5页
Flight Dynamics
关键词
高超声速巡航导弹
攻防对抗仿真
突防效能
作战效能
hypersonic cruise missile
combat engagement simulation
penetration effectiveness
combat elfectiveness