Vitiello Federica, Causa Flavia, Opromolla Roberto, Fasano Giancarmine
Department of Industrial Engineering, University of Naples "Federico II", P.le Tecchio 80, 80125 Naples, Italy.
Sensors (Basel). 2021 May 21;21(11):3582. doi: 10.3390/s21113582.
This paper describes a calibration technique aimed at combined estimation of onboard and external magnetic disturbances for small Unmanned Aerial Systems (UAS). In particular, the objective is to estimate the onboard horizontal bias components and the external magnetic declination, thus improving heading estimation accuracy. This result is important to support flight autonomy, even in environments characterized by significant magnetic disturbances. Moreover, in general, more accurate attitude estimates provide benefits for georeferencing and mapping applications. The approach exploits cooperation with one or more "deputy" UAVs and combines drone-to-drone carrier phase differential GNSS and visual measurements to attain magnetic-independent attitude information. Specifically, visual and GNSS information is acquired at different heading angles, and bias estimation is modelled as a non-linear least squares problem solved by means of the Levenberg-Marquardt method. An analytical error budget is derived to predict the achievable accuracy. The method is then demonstrated in flight using two customized quadrotors. A pointing analysis based on ground and airborne control points demonstrates that the calibrated heading estimate allows obtaining an angular error below 1°, thus resulting in a substantial improvement against the use of either the non-calibrated magnetic heading or the multi-sensor-based solution of the DJI onboard navigation filter, which determine angular errors of the order of several degrees.
本文描述了一种校准技术,旨在联合估计小型无人机系统(UAS)的机载和外部磁干扰。具体而言,目标是估计机载水平偏差分量和外部磁偏角,从而提高航向估计精度。这一结果对于支持飞行自主性很重要,即使在存在显著磁干扰的环境中也是如此。此外,一般来说,更精确的姿态估计对地理参考和测绘应用有益。该方法利用与一个或多个“副”无人机的协作,并结合无人机对无人机的载波相位差分全球导航卫星系统(GNSS)和视觉测量,以获得与磁场无关的姿态信息。具体来说,在不同航向角获取视觉和GNSS信息,并将偏差估计建模为通过列文伯格-马夸尔特方法求解的非线性最小二乘问题。推导了一个解析误差预算来预测可达到的精度。然后使用两架定制的四旋翼无人机在飞行中演示了该方法。基于地面和空中控制点的指向分析表明,校准后的航向估计允许获得低于1°的角误差,从而相对于使用未校准的磁航向或大疆机载导航滤波器基于多传感器的解决方案有了显著改进,后者确定的角误差为几度量级。