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Cislunar space awareness is of increasing interest to the internationalcommunity as Earth-Moon traffic is projected to increase. This raises theproblem of placing satellites optimally in a constellation to providesatisfactory coverage for said traffic. The Circular Restricted 3 Body Problem(CR3BP) provides promising periodic orbits in the Earth-Moon rotating frame fortraffic monitoring. This work converts a spatially and temporally varyingtraffic coverage requirement into an integer linear programming problem,attempting to minimize the number of satellites required for the requestedcoverage.

Cislunar Satellite Constellation Design Via Integer Linear Programming