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Research and Experiment on System Level Calibration Method of Fiber Optic Strapdown Inertial Navigation System

机译:光纤捷联惯导系统系统级标定方法的研究与实验

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An analysis is made to the zero bias, installation errors and scale factor propagation laws of a fiber optic strapdown inertial measurement unit from the systematic perspective, aiming to solve the problem that a certain type of fiber optic strapdown inertial navigation system requires a high precision turntable and is affected the rubber shock absorber in the conventional discrete calibration. A four-position rotation stop is conducted around X, Y, Z gyro sensitivity axes to excite the error parameters of fiber optic gyros and accelerometers, thus achieving systematic calibration of the fiber optic strapdown inertial measurement unit. By comparing with the conventional discrete calibration method with gyro rate calibration and twelve-position calibration of accelerometers, an undamped navigation swing test of the same batch is carried out on the calibrated error parameters. The test indicates that when the navigation test is performed with the systematic calibration results, the velocity errors, position errors and positioning error output by the system are smaller than those derived from the navigation test with the discrete calibration results.
机译:从系统的角度对光纤捷联惯性测量装置的零偏,安装误差和比例因子传播规律进行了分析,旨在解决某类光纤捷联惯性导航系统需要高精度转台的问题。并在常规离散校准中影响了橡胶减震器。围绕X,Y,Z陀螺仪灵敏度轴进行四位置旋转停止,以激发光纤陀螺仪和加速度计的误差参数,从而实现对光纤捷联惯性测量单元的系统校准。通过与传统的带有陀螺仪率校准和加速度计的十二位校准的离散校准方法进行比较,对校准后的误差参数进行了同一批次的无阻尼导航摆幅测试。该测试表明,当使用系统的校准结果执行导航测试时,系统输出的速度误差,位置误差和定位误差要小于使用离散校准结果的导航测试得出的速度误差,位置误差和定位误差。

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