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On-board correction of systematic error of Earth sensors

机译:车载校正地球传感器的系统误差

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Infrared Earth sensors are used in spacecraft for attitude sensing. Their accuracy is limited by systematic and random errors. Dominant sources of systematic errors are analyzed for a typical scanning infrared Earth sensor used in a remote-sensing satellite in a 900-km Sun-synchronous orbit. The errors considered arise from seasonable variation of infrared radiation; oblate shape of the Earth; ambient temperature of sensors; changes in spin/scan period; and misalignment of the axis of the sensors. Simple relations are derived using least-squares curve fitting for onboard correction of these errors. With these, it is possible to improve the accuracy of attitude determination by eight fold and achieve performance comparable to ground-based post-facto attitude computation.
机译:红外地球传感器在航天器中用于姿态感测。它们的准确性受到系统和随机误差的限制。对于在900公里太阳同步轨道上的遥感卫星中使用的典型扫描红外地球传感器,分析了系统误差的主要来源。所考虑的错误是由于红外辐射的季节性变化引起的;地球的扁圆形状;传感器的环境温度;自旋/扫描周期的变化;以及传感器的轴未对准。使用最小二乘曲线拟合导出简单关系,以对这些误差进行车载校正。利用这些,可以将姿态确定的精度提高八倍,并获得与基于地面的事后姿态计算可比的性能。

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