| 初始对准中常规六状态卡尔曼滤波器的应用 |
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| 引用本文： | 熊勇辉,潘宏侠. 初始对准中常规六状态卡尔曼滤波器的应用[J]. 机械管理开发, 2006, 0(1): 60-61 |
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| 作者姓名： | 熊勇辉 潘宏侠 |
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| 作者单位： | 中北大学自动控制系,山西,太原,030051;中北大学自动控制系,山西,太原,030051 |
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| 摘 要： | 建立了常规六状态滤波器误差方程,进行了kalman滤波仿真,得到航向、姿态角误差和陀螺漂移误差量,进行补偿。仿真结果显示常规滤波器在初始对准中取得了较好的效果。
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| 关 键 词： | 对准 常规卡尔曼滤波 惯性导航 |
| 文章编号： | 1003-773X（2006）01-0060-02 |
| 收稿时间： | 2005-08-30 |
| 修稿时间： | 2005-08-30 |
Application of Normal Six States Kalman Filter in the Initial Alignment |
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| Xiong Yonghui,Pan Hongxia. Application of Normal Six States Kalman Filter in the Initial Alignment[J]. Mechanical Management and Development, 2006, 0(1): 60-61 |
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| Authors: | Xiong Yonghui Pan Hongxia |
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| Affiliation: | Xiong Yonghui Pan Hongxia |
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| Abstract: | This text sets up error equations of mormal six states Kalman filter,realizes computer simulation to get estimation of heading,attitude and gyro drift according to the data of micro-silicon gyroscope.The simulation result indicates that it has good effects on the initial alignment. |
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| Keywords: | Alignment Normal Kalman filtering Inertial navigation |
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