Xiang Zhiyi, Wang Qi, Huang Rong, Xi Chongbin, Nie Xiaoming, Zhou Jian
Appl Opt. 2021 Sep 10;60(26):7869-7877. doi: 10.1364/AO.430866.
With the advantages of high velocity measurement accuracy and fast dynamic response, the laser Doppler velocimeter (LDV) is expected to replace the odometer to be combined with a strapdown inertial navigation system (SINS) to form a higher precision integrated navigation system. However, LDV scale factor error and misalignment angles between LDV and inertial measurement unit will affect the accuracy of navigation. Considering that not all global navigation satellite system (GNSS) receivers can directly provide velocity information and current mainstream calibration methods are sensitive to the measurement noise and outliers of velocity and position information, a robust calibration method aided by GNSS is proposed in this paper, which is based on position observation. Different from current popular calibration methods, the attitude information of the GNSS/SINS integrated navigation system obtained by an adaptive Kalman filter is used to construct the observation vector together with LDV velocity outputs and GNSS position outputs in this method. The LDV scale factor error and the misalignment angle are determined by the ratio of two observation vector modulus and the Davenport's q-method method, respectively. The accuracy and robustness of the calibration method are verified by one vehicle test with normal GNSS signals and one vehicle test with GNSS signals with outliers. And the horizontal position error of dead reckoning of the calibrated LDV/SINS integrated system are less than 0.0314% and 0.1033% of the mileage, respectively.
激光多普勒测速仪(LDV)具有测速精度高、动态响应快的优点,有望取代里程计与捷联惯性导航系统(SINS)相结合,形成更高精度的组合导航系统。然而,LDV的比例因子误差以及LDV与惯性测量单元之间的失准角会影响导航精度。考虑到并非所有全球导航卫星系统(GNSS)接收机都能直接提供速度信息,且当前主流的校准方法对速度和位置信息的测量噪声及异常值较为敏感,本文提出一种基于位置观测的、由GNSS辅助的鲁棒校准方法。与当前流行的校准方法不同,该方法利用自适应卡尔曼滤波器获得的GNSS/SINS组合导航系统的姿态信息,与LDV速度输出和GNSS位置输出共同构建观测向量。LDV比例因子误差和失准角分别通过两个观测向量模的比值和达文波特q法确定。通过一次正常GNSS信号的车载试验和一次含异常值的GNSS信号的车载试验,验证了校准方法的准确性和鲁棒性。校准后的LDV/SINS组合系统航位推算的水平位置误差分别小于里程的0.0314%和0.1033%。