Zero Drift Regions and Control strategies around Triangular Libration point in the restricted Sun-Earth-Moon scenario

Abstract

Assume that a group of two or more satellites are ying close a given nominal trajectory around Earth-Moon triangular point, in such a way that, there is some freedom in the selection of the geometry of the constellation. We are interested in avoiding large variations of the mutual distances between spacecraft and controlling the conguration of the formation… (More)

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