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巡航导弹飞行捷径、高度及速度对突防影响的仿真研究

Emulational study on the effect on the cruise missile penetration by shortcut flight course, flight altitude and flight velocity

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【作者】 虞蕾; 杜娟; 赵红; 赵宗涛;

【Author】 YU Lei~(1,2), DU Juan~2, ZHAO Hong~3, ZHAO Zong-tao~(1,2) ( 1.Department of Computer Science, Northwest University, Xi’an Shanxi 710069, China; 2.Division of Computer Science, Xi’an Research Inst. of Hi-Tech., Xi’an Shanxi 710025, China; 3.Department of Computer Science, Northwest Polytechnical University, Xi’an Shanxi 710072, China)

【机构】 西北大学计算机科学系; 西安高技术研究所计算机室; 西北工业大学计算机学院; 西北大学计算机科学系 陕西西安710069; 陕西西安710025; 陕西西安710072; 陕西西安710069; 陕西西安710025;

【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.

【Abstract】 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, mathema-(tical) 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.)

【关键词】 巡航导弹; 突防; 仿真;
【Key words】 cruise Missile; penetration; route planning;
【基金】 国防基金项目(EP010240-10)
  • 【文献出处】 延边大学学报(自然科学版) ,Journal of Yanbian University (Natural Science Edition) , 编辑部邮箱 ,2005年03期
  • 【分类号】TJ761
  • 【被引频次】7
  • 【下载频次】380
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