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Spin-Axis Attitude Determination from Earth Chord-Angle Variations for Geostationary Satellites

机译:对地静止卫星从地球弦角变化确定自旋轴姿态

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Spin stabilization offers a straightforward and robust concept for spacecraft attitude control. The spin-axisnattitude determination is usually accomplished by means of sun- and Earth-sensor measurements. This papernexplores techniques for spin-axis attitude determination using only Earth-sensor data. An immediate attitudendetermination can be achieved by straightforward geometrical arguments based on the extremes of the chord-anglenvariations over the orbit. Furthermore, an effective least-squares approach is presented that employs a number ofnequidistant chord-angle measurements collected during one orbital revolution. The adopted measurement model isnfavorable for reducing the adverse effects of systematic errors. Finally, a few explicit approaches are offered fornreconstructing the most important biases. The application of these techniques is illustrated by means of actualntelemetry data from the METEOSAT second-generation satellite MSG-2.
机译:自旋稳定为航天器姿态控制提供了一个简单而强大的概念。通常通过太阳和地球传感器的测量来确定自旋轴的高度。本文探讨了仅使用地球传感器数据确定自旋轴姿态的技术。通过基于轨道上弦-角度变化的极端值的简单几何参数,可以立即确定姿态。此外,提出了一种有效的最小二乘方法,该方法采用了在一次轨道旋转期间收集的许多等距弦角测量值。采用的测量模型不利于减少系统误差的不利影响。最后,提供了一些明确的方法来重建最重要的偏差。借助于来自METEOSAT第二代卫星MSG-2的实际遥测数据说明了这些技术的应用。

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