载机与巡航弹最优突防策略  

Optimal Penetration Maneuver of Fighter Plane and Cruise Missile

作　　者：涂永梅[1] 南英[1] 彭云[1] 李延其[1] 

机构地区：[1]南昌航空工业学院航空与机械工程学院,南昌330063

出　　处：《弹道学报》2007年第3期41-43,共3页Journal of Ballistics

摘　　要：研究了载机与巡航弹对抗拦截弹的最佳突防策略,提出了几种突防方案.针对机动变轨技术、抛射诱饵以及综合以上2种突防方案,建立数学仿真模型.采用数值仿真,比较了各种对抗与拦截飞行轨迹.基于攻防双方的数值仿真统计突防概率并对其进行比较,确定出综合采用机动变轨技术与抛射诱饵为最佳突防策略.The optimal penetration maneuver of planes and cruise missile which confront intercepting missiles was studied. Several penetration schemes were given, such as trajectory maneuver, decoy technology and integration of the above penetration schemes. The mathematical models of numerical simulation were established for the three penetration schemes and intercepting missiles. Several penetration flight trajectories were compared. Based on a great deal of numerical simulations of attack-defense, penetration probabilities were computed and compared. The integration of trajectory maneuver and decoy technology is regarded as the optimal penetration maneuver by analyzing penetration probabilities.

关 键 词：载机 突防概率 数值仿真 

分 类 号：TJ76[兵器科学与技术—武器系统与运用工程]