NASA Double Asteroid Redirection Test (DART) Trajectory Validation and Robutness
NASA Double Asteroid Redirection Test (Dart) Trajectory Validation and Robustness
Mars, Phobos, and Deimos Sample Return Enabled by ARRM Alternative Trade Study Spacecraft
Interplanetary Low-Thrust Design Using Proximal Policy Optimization
Improved Propulsion Modeling for Low-Thrust Trajectory Optimization
Identifying Accessible Near-Earth Objects For Crewed Missions With Solar Electric Propulsion
Global Optimization of Low-Thrust Interplanetary Trajectories Subject to Operational Constraints