| 高级惯性参考球在导弹精度鉴定中的作用 |
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| 引用本文： | 宋旭滨,解诒哲.高级惯性参考球在导弹精度鉴定中的作用[J].航天控制,1991(Z1). |
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| 作者姓名： | 宋旭滨 解诒哲 |
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| 作者单位： | 北京控制器件研究所，北京控制器件研究所 |
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| 摘 要： | 文章介绍了高级惯性参考球的结构特点,给出连续自对准和自校准的部分研究结果,其中的软件部分可方便地用在导弹性能测量系统(MPMS)中。文章还给出了两套惯性测量装置的评价方法的数学公式,且建议采用新的数据处理方法:卡尔曼回归算法。最后,分析了采用MPMS方法的可能优点。
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| 关 键 词： | 高级惯性基准球 精度分析 惯性测量装置 |
AN APPLICATION OF AIRS TO ACCURACY EVALUATION OF MISSILES |
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| Song Xubing Xie Yighe Beijing Control Device Research Institute.AN APPLICATION OF AIRS TO ACCURACY EVALUATION OF MISSILES[J].Aerospace Control,1991(Z1). |
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| Authors: | Song Xubing Xie Yighe Beijing Control Device Research Institute |
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| Institution: | Song Xubing Xie Yighe Beijing Control Device Research Institute |
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| Abstract: | The structure features of AIRS (Advanced Inertial Reference System) are presented in the paper. Some results related to the self-alignment and self-calibration researches have been obtained, among which the software parts of them can easily be used to missile performance measurement system (MPMS). The paper also presents the two set of mathematioal formulas for evaluating IMD (inertial measurement Device), and a new data processing method, the kalman-based regression algorithm, is recommended. |
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| Keywords: | Advanced inertial reference sphere Accuracy analysis Inertial measurement unit |
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