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Laser Guided Space Interferometer (LGSI)

A concept for a CubeSat/SmallSat mission for a ~3 km baseline optical interferometer in space.

An example of orbits for the free-flying componenets of the LGSI: mirrors, combiner, and laser guide star (LGS). The orbits are propagrated using poliasto with Sun as a perturbing body. The exmple includes precomputed manuevers to keep mirros, aligned, increase uv coverage, and repoint the LGS.

A very simple optical simualtion to very optimistically estimate the required number of photons from a target star.