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A Navigation Application and Calibration Method for Gyroscope Free Strap-Down Inertial Navigation System

机译:无陀螺捷联惯性导航系统的导航应用及标定方法

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摘要

The accuracy of a gyroscope free INS is deeply affected by the bias, scale factor and misalignment. However, these error parameters can be obtained by calibration. This paper presents two research issues. The first is an improvement to the original six-accelerometer model to achieve more realistic performance. The second is a novel calibration method for the proposed six-accelerometer INS. In navigation applications the improved model will determine the rotational and translational acceleration of a vehicle from the six accelerometer outputs. The proposed calibration method will decrease the system error to enhance the navigation performance.
机译:不含陀螺仪的INS的精度受偏置,比例因子和未对准的影响很大。但是,这些误差参数可以通过校准获得。本文提出了两个研究问题。首先是对原始六加速度计模型的改进,以实现更逼真的性能。第二种是建议的六加速度计INS的新颖校准方法。在导航应用中,改进的模型将根据六个加速度计输出确定车辆的旋转和平移加速度。所提出的校准方法将减少系统误差以增强导航性能。

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