An LQR controller for formation flight near halo orbits is computed for a single orbital period and extended to all later times by a fixed rotation, with simulations showing up to 40% less fuel use than an impulsive baseline.
Earth-M oon Near Rectilinear Halo and Butterfly Orbits for Lunar Surface Exploration,
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LQR Design For Formation Flying Near Halo Orbits Exploiting Quasi-Periodic Symmetry In Toroidal Coordinates
An LQR controller for formation flight near halo orbits is computed for a single orbital period and extended to all later times by a fixed rotation, with simulations showing up to 40% less fuel use than an impulsive baseline.