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Star sensor on-orbit calibration using Extended Kalman Filter

机译:使用扩展卡尔曼滤波器的恒星传感器在轨校准

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A sequential on-orbit calibration method based on Extended Kalman Filter was proposed in this paper. Considering the distortion feature of most star camera optics lens, focal length of star sensor and first order radial distortion coefficient were calibrated separately with radial aberration be considered only. Results from Extended Kalman Filter were optimum estimation for calibration parameters founded on principle that Inter-Star Angles are invariants, whether measured in image frame or inertial frame. The simulation results showed that this method could respond to changes of internal parameters very soon, which would do perfectly in working situation where real time was needed. When the standard deviation of star positional noise is set to 0. 05 pixels, accuracy of 1.2 arc-second could be obtained by this scheme, and it can meet the accuracy demand given to on-orbit calibration of star sensor.
机译:提出了一种基于扩展卡尔曼滤波的序列在轨定标方法。考虑到大多数星形摄像机光学透镜的畸变特征,仅考虑径向像差分别校准星形传感器的焦距和一阶径向畸变系数。扩展卡尔曼滤波器的结果是对校准参数的最佳估计,其依据是星际角是不变的原理,无论是在图像帧中还是在惯性帧中进行测量。仿真结果表明,该方法能够很快响应内部参数的变化,在需要实时的工作情况下效果最佳。当恒星位置噪声的标准偏差设置为0. 05像素时,该方案可获得1.2弧秒的精度,可以满足恒星传感器在轨定标的精度要求。

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