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A Fast Initial Alignment Method for SINS on Stationary Base

机译:静止基座上捷联惯导的快速初始对准方法

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In case of initial self-alignment for SINS on stationary base, when the level accelerometer outputs are taken as the measurement value for Kalman filter, the convergence speed of azimuth misalignment angle is limited by the observability of SINS. A fine alignment method for SINS is introduced firstly, which can do the accelerometer-based leveling alignment and gyro-based heading alignment simultaneously. The observability analysis by Singular Value Decomposition for this method shows that, the degree of observability of SINS is improved by adding observable extern information. Based on the analysis, a fast initial alignment method is proposed, which employs a reduced order alignment Kalman filter and takes both the level accelerometer outputs and east gyroscope output as the measurement value. Besides, the model error compensation method is given. Simulation and experimental comparison results between this fast alignment method and traditional one illustrate that, the convergence speed of azimuth misalignment angle is improved greatly with good real-time performance.
机译:在静止基座上进行SINS初始自对准的情况下,当将水平加速度计输出作为Kalman滤波器的测量值时,方位角未对准角的收敛速度受到SINS的可观察性的限制。首先介绍了一种捷联惯导系统的精确对准方法,该方法可以同时进行基于加速度计的水平对准和基于陀螺仪的航向对准。通过奇异值分解的可观察性分析表明,通过添加可观察的外部信息可以提高SINS的可观察度。在分析的基础上,提出了一种快速初始对准方法,该方法采用降阶对准卡尔曼滤波器,并以水平加速度计输出和东陀螺仪输出作为测量值。此外,给出了模型误差补偿方法。通过仿真和实验比较,表明该方法与传统方法相比,方位失准角的收敛速度有了较大的提高,具有较好的实时性。

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