| 巡航导弹飞行捷径、高度及速度对突防影响的仿真研究 |
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| 引用本文： | 虞蕾 杜娟 赵红 赵宗涛. 巡航导弹飞行捷径、高度及速度对突防影响的仿真研究[J]. 延边大学学报(自然科学版), 2005, 31(3): 216-219 |
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| 作者姓名： | 虞蕾 杜娟 赵红 赵宗涛 |
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| 作者单位： | [1]西北大学计算机科学系,陕西西安710069 [2]西安高技术研究所计算机室,陕西西安710025 [3]西北工业大学计算机学院,陕西西安710072 |
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| 基金项目： | 国防基金项目（EP010240-10） |
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| 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．
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| 关 键 词： | 巡航导弹 突防 仿真 |
| 文章编号： | 1004-4353(2005)03-0216-04 |
| 收稿时间： | 2005-06-21 |
| 修稿时间： | 2005-06-21 |
Emulational study on the effect on the cruise missile penetration by shortcut flight course, flight altitude and flight velocity |
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| YU Lei, DU Juan, ZHAO Hong, ZHAO Zong-tao. Emulational study on the effect on the cruise missile penetration by shortcut flight course, flight altitude and flight velocity[J]. Journal of Yanbian University (Natural Science), 2005, 31(3): 216-219 |
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| Authors: | YU Lei DU Juan ZHAO Hong ZHAO Zong-tao |
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| Affiliation: | 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 Shanwi 710025, China ; 3. Department of Computer Science, Northwest Polytechnical University, Xi ' an Shanxi 710072, China |
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| 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.) |
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| Keywords: | cruise Missile penetration route planning |
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