Microsatellite constellation for earth observation missions

A. Sezer, Orhan Çelikkaya, B. Hassoy
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引用次数: 4

Abstract

Recent technological advances in satellite miniaturization, directed efforts in earth observation towards microsatellite constellations. Ultimate goals of Earth observation satellite missions are having maximum number of images with high quality and maximum orbital performance such as maximum coverage and minimum revisit time. These goals can be achieved by microsatellite constellations. In this study, different conceptual constellation alternatives were analysed to optimise daily coverage and revisit times. In house tools were used for propagating the orbit and swath coverage modelling. Satellite potential swath is calculated on equidistant map projection using sub-satellite point, ground-track heading and off-nadir viewing angle.
用于地球观测任务的微卫星星座
卫星小型化方面的最新技术进步,将对地观测的努力导向微型卫星星座。地球观测卫星任务的最终目标是获得最多数量的高质量图像和最大的轨道性能,如最大的覆盖范围和最短的重访时间。这些目标可以通过微卫星星座来实现。在本研究中,分析了不同概念星座备选方案,以优化每日覆盖和重访时间。内部工具用于传播轨道和带状覆盖模型。利用星下点、地面航迹航向和离最低点视角在等距地图投影上计算卫星势条。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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