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Consistent calibration of magnetometers for nonlinear attitude determination

机译:磁力计的一致校准,用于确定非线性姿态

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摘要

Three-axis magnetometers (TAMs) have been widely utilized as the cornerstone of integrated navigation (IN) and attitude determination (AD) in many aerospace systems. However, accurate navigation and AD demands for precise calibration of TAM. For this purpose, a complete TAM calibration process is presented in the current research to compensate all of the key errors. In this regard, a hyper least square (HyperLS) estimator is extended for accurate and consistent ellipsoid fitting problem of TAM calibration. Subsequently, the calibrated TAM is utilized for real time attitude determination via non-linear colored noise filters of extended Kalman filter, simplex unscented Kalman filter (SUKF) and cubature Kalman filter. Effectiveness of the proposed calibration scheme is investigated through implementation on a Honeywell HMC5883L magnetometer. Comparative study of the results with those of well-known methods of strict ellipsoid and the three-step algorithm demonstrates the suitability of the HyperLS and SUKF in terms of accessible estimation accuracy. (C) 2015 Elsevier Ltd. All rights reserved.
机译:三轴磁力计(TAM)已被广泛用作许多航空系统中集成导航(IN)和姿态确定(AD)的基石。但是,准确的导航和AD要求对TAM进行精确校准。为此,目前的研究提出了完整的TAM校准过程,以补偿所有关键误差。在这方面,扩展了超最小二乘(HyperLS)估计器,以实现TAM校准的准确和一致的椭球拟合问题。随后,将校准的TAM通过扩展的卡尔曼滤波器,单纯味无味卡尔曼滤波器(SUKF)和培养箱卡尔曼滤波器的非线性彩色噪声滤波器用于实时姿态确定。通过在霍尼韦尔(中国)HMC5883L磁力计上实施,研究了提出的校准方案的有效性。将结果与严格的椭球体的著名方法和三步算法进行的比较研究证明,HyperLS和SUKF在可访问估计精度方面是合适的。 (C)2015 Elsevier Ltd.保留所有权利。

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