State Transition Tensors for Continuous-Thrust Control of Three-Body Relative Motion
Solar-Sail Quasi-Periodic Orbits in the Sun–Earth System
Optimization-Aided, Low-Energy Transfers via Vertical Instability Around Earth–Moon
Low-Thrust Trajectory Design with Successive Convex Optimization for Libration Point Orbits
High-Resolution Global Point Mascon Models for the Moon
Dynamics Near the Three-Body Libration Points via Koopman Operator Theory
Dumping Momentum on the Lunar Gateway Using a Robotically Steerable Solar Sail
Bearings-Only Guidance in Cis-Lunar Rendezvous