| 空间导弹快速拦截最优发射轨道设计 |
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| 引用本文： | 方飞,和兴锁,张亚锋. 空间导弹快速拦截最优发射轨道设计[J]. 山西大学学报(自然科学版), 2006, 29(2): 158-161 |
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| 作者姓名： | 方飞 和兴锁 张亚锋 |
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| 作者单位： | 西北工业大学,工程力学系,陕西,西安,710072 |
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| 摘 要： | 根据轨道动力学的理论,建立空间导弹快速拦截模型,求解轨道参数.根据飞行时间最短,燃料消耗最小的性能指标进行优化设计.然后寻找这两个指标的综合最优值,最后提出区域拦截的概念.本文解决的核心问题是确定最优拦截轨道和拦截点,找到卫星位置和最优拦截点之间的对应关系,实现空间导弹对卫星的实时拦截.
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| 关 键 词： | 空间导弹 能量最小 时间最短 轨道参数 区域拦截 |
| 文章编号： | 0253-2395(2006)02-0158-04 |
| 收稿时间： | 2005-06-18 |
| 修稿时间： | 2005-10-09 |
The Optimization Design of the Space Missile Intercepting |
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| FANG Fei,HE Xing-suo,ZHANG Ya-feng. The Optimization Design of the Space Missile Intercepting[J]. Journal of Shanxi University (Natural Science Edit, 2006, 29(2): 158-161 |
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| Authors: | FANG Fei HE Xing-suo ZHANG Ya-feng |
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| Abstract: | The model of the space missile intercepting quickly was built and the orbit parameters were solved based on the theories of the orbit dynamics,second time and energies optimization,respectively.The integrative optimization of these two indexes was figured out.And the concept of district intercepting was introduced.The kernel problem of this research was the design of optimization orbit.According to the method,the satellite can be intercepted by the space missile in time. |
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| Keywords: | space missile minimum energy shortest time orbit parameter district intercepting |
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