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Attitude calculating for a new strap-down inertial navigation system based on angular accelerometers

机译:基于角加速度计的新型捷联惯性导航系统的姿态计算

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This paper introduces an attitude updating method based on a new structure of gyroscope-free inertial navigation system(GFINS), in which the angular accelerometers are used to take the place of gyroscopes. For this new structure of GFINS, a new mathematical model is developed to determine the general three-dimensional motion of body segments. The mathematical model is mainly based on the direction cosine matrix. A second-order differential equation which is represented by angular acceleration should be calculated to solve this problem using the fourth order Runge-Kutta method combining with the interpolation method. Furthermore, the final result of this approach is shown by applying the mathematical model to some simulation data generated by the trajectory generator. The simulation results indicate that the mathematical model has a good performance.
机译:介绍了一种基于无陀螺惯性导航系统(GFINS)新结构的姿态更新方法,该方法采用角加速度计代替陀螺仪。对于GFINS的这种新结构,开发了一种新的数学模型来确定人体节段的一般三维运动。数学模型主要基于方向余弦矩阵。为了解决这个问题,应使用四阶Runge-Kutta方法和插值方法来计算以角加速度表示的二阶微分方程。此外,通过将数学模型应用于由轨迹生成器生成的一些模拟数据,可以显示该方法的最终结果。仿真结果表明该数学模型具有良好的性能。

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