| 火箭惯性测速定位的简易基点计算方法 |
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| 引用本文： | 李振涛.火箭惯性测速定位的简易基点计算方法[J].航天控制,1990(2). |
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| 作者姓名： | 李振涛 |
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| 作者单位： | 北京航天自动控制研究所 |
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| 摘 要： | 本文介绍了火箭惯性测速定位的一种新的计算方法。计算结果表明,该方法既能提高计算精度,也能使计算量减少到原来的1/(10)。并且使用灵活,可输出任意指定时刻的飞行状态参数。
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| 关 键 词： | 制导 制导方程 计算方法 |
A SIMPIE BASE-POINT COMPUTATION METHOD FOR MEASURING INERTIAL VELOCITY AND POSITION OF ROCKET |
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| Li Zhentao Beijing Aerospace Automatic Control Institute.A SIMPIE BASE-POINT COMPUTATION METHOD FOR MEASURING INERTIAL VELOCITY AND POSITION OF ROCKET[J].Aerospace Control,1990(2). |
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| Authors: | Li Zhentao Beijing Aerospace Automatic Control Institute |
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| Institution: | Li Zhentao Beijing Aerospace Automatic Control Institute |
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| Abstract: | This paper presents a new calculation method that is used to measure inertial velocity and position for rocket. The calculated results have shown that this method can enhance calculating accuracy and reduce the amount of calculation to 1/10 of that of usual one. This method possesses flexibitity in use and can give out parameters of the fight state at any given time. |
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| Keywords: | Guidance Guidance equation Calculation method |
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