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Research on Airborne Passive Location Based on Extend Kalman Filter with Control Inputs

机译:基于控制输入扩展卡尔曼滤波的机载无源定位研究

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This paper describes the principle and method of traditional Kalman Filter (KF) algorithm and Extended Kalman Filter (EKF) with control inputs. An airborne 3D model of passive location system is established. And then the linearization of the nonlinear observation model and the steps and formulas of the recursive filtering estimation with the EKF with control inputs are derived. Finally, the using of the EKF with control inputs algorithm to solve passive location method based on the azimuth angle and pitching angle information is verified by computer simulation. The results show that this method is a new process with practical engineering significance.
机译:本文介绍了具有控制输入的传统卡尔曼滤波器(KF)算法和扩展卡尔曼滤波器(EKF)的原理和方法。建立了被动定位系统的机载3D模型。然后推导了非线性观测模型的线性化,并利用带有控制输入的EKF推导了递归滤波估计的步骤和公式。最后,通过计算机仿真验证了EKF与控制输入算法在基于方位角和俯仰角信息的基础上求解无源定位方法的有效性。结果表明,该方法是一种具有实际工程意义的新方法。

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