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In-flight Heading Estimation of Strapdown Magnetometers using Particle Filters

机译:使用粒子滤波器的捷联式磁力计的飞行航向估计

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摘要

This paper presents a real-time heading estimation algorithm using IMU and strapdown magnetometer without any other external heading reference. To calibrate the magnetic deviation, sensor errors caused by hard iron effect and initial heading of strapdown magnetometers are considered. In our approach, sensor output distortion due to the soft iron effect is ignored, which is relatively small. First, for the estimation of heading angle, system and measurement model is derive, which is nonlinear. Then particle filter and extended Kalman filter is introduced for performance comparison. The proposed algorithm for the integration of IMU and magnetometer is verified via numerical simulation in Matlab. Simulation result demonstrates accurate heading estimation error within 1 degree for both algorithms when there exists small initial heading error and hard iron effect, yet particle filter provides more robust and precise result than the extended Kalman filter in case the initial heading error and biases are large.
机译:本文提出了使用IMU和捷联式磁力计的实时航向估计算法,而没有任何其他外部航向参考。为了校准磁偏差,考虑了由硬铁效应和捷联式磁力计的初始航向引起的传感器误差。在我们的方法中,由于软铁效应而引起的传感器输出失真被忽略,这相对较小。首先,为了估计航向角,推导了非线性的系统和测量模型。然后引入粒子滤波器和扩展卡尔曼滤波器进行性能比较。在Matlab中通过数值仿真验证了所提出的IMU和磁力计集成算法。仿真结果表明,当初始航向误差和铁质效应较小时,两种算法的航向估计误差均在1度以内,但在初始航向误差和偏差较大的情况下,粒子滤波器比扩展卡尔曼滤波器具有更强的鲁棒性和精确度。

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