基于有限脉冲响应模型的飞机磁场补偿方法
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    摘要:

    通过分析飞机磁场数学模型,将飞机磁场表示成方向余弦与其乘积项的函数。鉴于模 型参数之间存在很强的复共线性,提出了基于有限脉冲响应模型飞机磁场补偿方法。该方法 将光泵磁强计和三轴磁强计的输出作为有限脉冲响应模型的输入,由带通滤波器提取信号中 的变化成分,再用最小方差估计有限脉冲响应模型参数,并利用有限脉冲响应模型参数计算飞 机磁场。从测量总磁场中减去飞机磁场,可得到目标信号磁场数据。最后通过计算机仿真验 证了该磁场补偿方法的有效性。

    Abstract:

    By analysis of a mathematic model of aircraft magnetic field, the airp lane magnetic field model was expressed by the direction cosine and its product terms. It was difficult to estimate the model parameters by using conventional m ethods due to the model collinearity, so a new compensation method using the fin ite impulse response model was proposed. The outputs of optical pumping magnetom eters and threeaxial magnetometers were used as the inputs of finite impulse r e sponse model. The bandpass filter was used to extract the variation magnetic f i eld, and the minimal variance was employed to estimate parameters of the finite impulse response model. The airplane magnetic field data was obtained by using p arameters of finite impulse response model. The total magnetic field data subtra cted by the airplane magnetic field data gives the detected object magnetic data . Finally, the method was validated by a computer simulation.

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