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INCLINED SUPER-GEOSTATIONARY EARTH ORBIT FOR IMPROVED SPACE SURVEILLANCE

机译:倾斜的超高地球轨道,改善了空间监视

摘要

PROBLEM TO BE SOLVED: To provide methods, systems and apparatus for an inclined super-geostationary earth orbit (super-GEO) for improved space surveillance.SOLUTION: Systems, methods, and apparatus for space surveillance are disclosed in the present specification. In one or more embodiments, the disclosed method involves a step of scanning, by at least one sensor on at least one satellite in an inclined super-geostationary earth orbit (super-GEO), a raster scan over a field of regard (FOR). In one or more embodiments, the scanning step is at a variable rate, and the variable rate is dependent upon a target dwell time for detecting a target of interest. In at least one embodiment, the target dwell time is a function of a range from at least one sensor to the target of interest and a function of a solar phase angle. In some embodiments, the axis of inclination of the inclined super-geostationary earth orbit (super-GEO) is a function of the solar phase angle.SELECTED DRAWING: Figure 1A
机译:解决的问题:提供用于倾斜的超地球静止地球轨道(super-GEO)的方法,系统和装置,以改善空间监视。解决方案:本说明书中公开了用于空间监视的系统,方法和装置。在一个或多个实施例中,所公开的方法包括以下步骤:通过倾斜的超对地静止地球轨道(super-GEO)中的至少一颗卫星上的至少一个传感器扫描视场(FOR)上的光栅扫描。 。在一个或多个实施例中,扫描步骤以可变速率进行,并且可变速率取决于用于检测感兴趣目标的目标停留时间。在至少一个实施例中,目标停留时间是从至少一个传感器到感兴趣目标的范围的函数,并且是太阳相位角的函数。在某些实施例中,倾斜的超对地静止地球轨道(super-GEO)的倾斜轴是太阳相位角的函数。图1A

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