| 基于空中发射点的在线诸元计算方法研究 |
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| 引用本文： | 鲜勇,王明海,陈燕梦.基于空中发射点的在线诸元计算方法研究[J].飞行力学,2007,25(4):58-60. |
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| 作者姓名： | 鲜勇 王明海 陈燕梦 |
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| 作者单位： | 1. 第二炮兵工程学院603教研室,陕西,西安,710025
2. 第二炮兵装备研究院,三所,北京,100075 |
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| 摘 要： | 现代战争的快节奏要求弹道导弹具有快速机动发射能力,采用伪卫星组合制导的弹道导弹随机快速发射需要诸元在线计算。提出了一种基于空中发射点的在线诸元计算方法,该方法具有计算量小、制导方法误差小的特点,可用于陆基机动弹道导弹或潜射弹道导弹的快速发射。
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| 关 键 词： | 空中发射点 在线诸元计算 制导方法误差 伪卫星 组合制导 |
| 文章编号： | 1002-0853（2007）04-0058-03 |
| 收稿时间： | 2006-08-21 |
| 修稿时间： | 2007-08-31 |
On an Online Data Computation Method Based on Air Launch Point |
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| XIAN Yong,WANG Ming-hai,CHENG Yan-meng.On an Online Data Computation Method Based on Air Launch Point[J].Flight Dynamics,2007,25(4):58-60. |
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| Authors: | XIAN Yong WANG Ming-hai CHENG Yan-meng |
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| Abstract: | The rapid maneuver capability and launch capability of ballistic missiles are requisite for the rapid rhythm on modern battlefields.Since online data computation is required by randomly and rapidly launching ballistic missiles in which pseudo-satellite integrated guidance is adopted,an online data computation method based on air launch points is proposed.The method has minor computer load and small guidance method error;therefore it can be used in rapid launching of land-based maneuver ballistic missiles or submarine-based ballistic missiles. |
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| Keywords: | space launch point online data computation guidance method error pseudo satellite integrated guidance |
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