Convex Model Predictive Control for Stationkeeping Control of Halo Orbits
We present a series of works using convex model predictive control for stationkeeping maneuver design of unstable halo orbits. One work proives fuel-optimal impulsive stationkeeping maneuvers as well as a safety plan thorughout the entire mission. The other work uses a solar sail propulsion model to generate the maneuvers. We validate our algorithms in simulations of the three-body Earth-Moon and Saturn-Enceladus systems demonstrating the effectiveness of our approach.
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Related Papers
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2025 March |
A Convex Optimization Approach to Solar Sail Station-Keeping Control in Halo Orbits
IEEE Aerospace Conference Big Sky, MT. (Accepted) |
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2025 March |
Contingency-Aware Station-Keeping Control of Halo Orbits
IEEE Aerospace Conference Big Sky, MT. (Accepted) |
People
Fausto Vega
Small Spacecraft and Navigation
Zac Manchester
Assistant Professor