| 民用飞机组合导航实际导航性能计算方法 |
| |
| 引用本文： | 宁亚锋,李文辉,谢轶俊,喻杰.民用飞机组合导航实际导航性能计算方法[J].航空电子技术,2020,51(2):50-54. |
| |
| 作者姓名： | 宁亚锋 李文辉 谢轶俊 喻杰 |
| |
| 作者单位： | 航空工业陕西飞机工业(集团)公司,汉中723213,中国航空无线电电子研究所,上海200241,中国航空无线电电子研究所,上海200241,中国航空无线电电子研究所,上海200241 |
| |
| 摘 要： | 提出了一种民用飞机组合导航实际导航性能计算方法，通过提取组合导航卡尔曼滤波器的误差协方差
矩阵，并对水平位置误差进行近似拟合，获得95% 的概率误差圆半径，即为组合导航实际导航性能。该方法
计算过程简单，易于实现，具有较强实用价值。
|
| 关 键 词： | 组合导航 实际导航性能 卡尔曼滤波 协方差矩阵 |
| 收稿时间： | 2020/1/17 0:00:00 |
| 修稿时间： | 2020/5/17 0:00:00 |
Actual Navigation Performance Calculation Algorithm for Integrated Navigation of
Civil Aircraft |
| |
| NING Ya-feng,LI Wen-hui,XIE Yi-jun,YU jie.Actual Navigation Performance Calculation Algorithm for Integrated Navigation of
Civil Aircraft[J].Avionics Technology,2020,51(2):50-54. |
| |
| Authors: | NING Ya-feng LI Wen-hui XIE Yi-jun YU jie |
| |
| Institution: | Shaanxi Aircraft Industry Group Corporation of Aviation Industry Corporation of China,Hanzhong 723213;China National Aeronautical Radio Electronics Research Institute, Shanghai 200241,China |
| |
| Abstract: | An ANP calculation algorithm is introduced for integrated navigation of civil aircrafts. Through extracting the error
covariance matrix of the integrated navigation kalman filter and approximately fitting the lateral position error, a circle radius can be
achieved with a 95% probability error. This is the introduced ANP of the integrated navigation. Such an algorithm is simple, easy to
implement and thus has a good practical value. |
| |
| Keywords: | integrated navigation actual navigation performance Kalman filter covariance matrix |
| 本文献已被 万方数据 等数据库收录！ |
| 点击此处可从《航空电子技术》浏览原始摘要信息 |
| 点击此处可从《航空电子技术》下载免费的PDF全文 |
|
