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Study of Independent Initial Alignment Based on Gyroscope Free Strapdown Inertial Navigation System

机译:基于陀螺仪的自由初始对准研究自由仪的自由表达惯性导航系统研究

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Conventional strapdown inertial navigation system is usually measured angular velocity with gyroscope and acceleration measuring a force signal with accelerometer for the initial alignment. GFSINS uses accelerometers that use the output from the ratio of force to solve the angular velocity instead of gyroscopes for the initial alignment. Based on a nine-accelerometer configuration and use of logarithmic algorithms give the solution of results of the acceleration and angular velocity, and analyze the principle of the initial alignment. In the static base, we analyze the initial alignment issues of GFSINS, use the kalman filter to reduce the accumulation of errors, and derive a kalman filter state equation and the prediction equation, at the same time do some simulations for the initial alignment.
机译:传统的挂轴惯性导航系统通常用陀螺仪测量角速度,并测量具有加速度计的力信号,用于初始对准。 GFSINS使用加速度计,该加速度计使用力的力与力比以解决角速度而不是陀螺仪的陀螺仪。基于九加速度计配置和使用对数算法的使用提供了加速度和角速度的结果,分析了初始对准的原理。在静态基础上,我们分析了GFSINS的初始对齐问题,使用卡尔曼滤波器来减少错误的累积,并导出卡尔曼滤波器状态方程和预测方程,同时对初始对准进行一些模拟。

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