本文首先介绍了卡尔曼滤波器，对各种导航数据进行信息融合，从而组成导航系统，以获取系统状态的最优估计。
This paper first introduced the kalman filter, to all sorts of navigation data information fusion, thus constituting navigation system, in order to get the optimal estimation system state.
介绍了利用卡尔曼滤波器估计弹道参数进而外推出敌方炮位的方法。
A method for estimating trajectory parameters by Kalman filter is introduced in this paper.
着重介绍了卡尔曼滤波器技术的原理、计算公式、模拟方法以及在组合导航系统中的应用。
The result of computer simulation in the GPS/INS integrated system shows that the algorithm is useful and effective with high effectiveness.
着重介绍了卡尔曼滤波器技术的原理、计算公式、模拟方法以及在组合导航系统中的应用。
The result of computer simulation in the GPS/INS integrated system shows that the algorithm is useful and effective with high effectiveness.
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