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Star sight with the charge coupled matrix, a method for detecting and application for the new setting of a spacecraft

机译:带有电荷耦合矩阵的星空,一种检测和应用航天器新环境的方法

摘要

For the analysis of the image of a faintly luminous objects in a rapid movement, the sighting device (1) receives information from coming from an inertial unit (18). It also has a cross section of a digital memory (17) of a window which contains the image of the object of the light. The tiles contained in windows realigned in succession, on the ccd matrix (3) are summed progressively and stored in a cross section of a digital memory (17) of the window. The sighting device (1) is also provided with calculation means (12) in order to determine the position of the image of the object of the light beam on the matrix (3) by calculation of the centres of gravity and the vector sum of these centres of gravity. & br / application to the resetting of an artificial satellite.
机译:为了分析快速运动中的微弱发光物体的图像,瞄准装置(1)从惯性单元(18)接收信息。它还具有窗口的数字存储器(17)的横截面,该窗口包含光物体的图像。 ccd矩阵(3)上连续重新对齐的窗口中包含的图块将逐步累加并存储在窗口的数字存储器(17)的横截面中。瞄准装置(1)还设有计算装置(12),以便通过计算重心和它们的矢量和来确定光束的图像在矩阵(3)上的位置。重心。 & br />应用于人造卫星的重置。

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