Cislunar Satellite Constellation Design via Integer Linear Programming
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Abstract
Cislunar space awareness is of increasing interest to the international community
as Earth-Moon traffic is projected to increase. This raises the problem of placing
satellites optimally in a constellation to provide satisfactory coverage for said
traffic. The Circular Restricted 3 Body Problem (CR3BP) provides promising periodic
orbits in the Earth-Moon rotating frame for traffic monitoring. This work
converts a spatially and temporally varying traffic coverage requirement into an
integer linear programming problem, attempting to minimize the number of satellites
required for the requested coverage.
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2023-08
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