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In this paper, dynamical systems theory and hybrid optimization techniques are integrated into a cohesive framework to design low-thrust trajectories for a small satellite to reach a highly out-of-ecliptic science orbit.
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This page is a summary of: Designing Low-Thrust Transfers to High-Inclination Science Orbits via Hybrid Optimization, Journal of Spacecraft and Rockets, May 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34980.
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