摘要
研究巡航导弹航迹规划中飞行捷径、高度及速度3个关键性因素,重点是通过仿真给出在其约束条件下巡航导弹突防的概率.通过大量实验和作战仿真得出单枚巡航导弹对歼击机火力单元突防的概率随航路捷径、高度以及速度变化的规律和数学模型.
Three key factors for cruise missile in route planning are studied, these are the shortcut flight course, flight altitude and flight velocity. It puts emphasis on the penetration probability for the cruise missile with computer simulation under restrictions. Based on many experiments and fighting simulation, mathematical model and relationship between of the penetration probability of single cruise missile by fighter plane＇s firepower units and three factors such as shortcut flight course, flight altitude and flight velocity were obtained.
出处
《延边大学学报（自然科学版）》
CAS
2005年第3期216-219,共4页
Journal of Yanbian University（Natural Science Edition）
基金
国防基金项目(EP010240-10)
关键词
巡航导弹
突防
仿真
cruise Missile
penetration
route planning
