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Cubature Kalman Filter In Initial Alignment of Large Heading Error In SINS

机译:Cubature卡尔曼滤波器在捷联惯导大航向误差的初始对准中

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Initial alignment is a key step in strapdown inertial navigation systems.In order to improve the accuracy of the navigation system with a large heading error,nonlinear error model is adopted and the cubature Kalman filter is applied to solve the filtering problem.We focus on the stationary basement,simulation results show good performance in case of nonlinear filtering problems and it is more efficient than EKF..
机译:初始对准是捷联惯性导航系统中的关键步骤。为了提高导航系统的精度,航向误差较大,采用非线性误差模型,并采用库曼卡尔曼滤波器来解决滤波问题。固定地下室,在非线性滤波问题下的仿真结果显示出良好的性能,并且比EKF效率更高。

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