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Research on precision windowed track mode for in-orbit calibration on star tracker

机译:星跟踪器在轨定标的精确窗口跟踪模式研究

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Implementation of an in-orbit calibration is an effective approach to reduce position error of individual star spot down to arcsec on star tracker. However, without knowledge of variance errors of some error sources, the reduction of such errors to what extent is unclear leading to in-orbit correction inefficiency. Based on Cramer Rao Lower Bound(CRLB) theory, we obtain the minimum variance error of position and make an accurate definition of precision windowed track mode for in-orbit calibration. After that, the error constraints on proper motion, velocity aberration, drift in focal length and other factors are studied in details. Imposing proper restrictions on those parameters, in-orbit correction of star tracker could approach CRLB accuracy.
机译:进行在轨校准是一种有效的方法,可以将单个恒星点的位置误差降低到恒星跟踪器上的arcsec。但是,在不知道某些误差源的方差误差的情况下,不清楚将这种误差减小到何种程度会导致在轨校正效率低下。基于Cramer Rao下界(CRLB)理论,我们获得了位置的最小方差误差,并为在轨定标精确定义了精确窗口跟踪模式。之后,详细研究了误差对适当运动,速度像差,焦距漂移和其他因素的限制。通过对这些参数施加适当的限制,恒星跟踪仪的在轨校正可能会接近CRLB的精度。

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