Low-Thrust Transfers from Distant Retrograde Orbits to L2 Halo Orbits in the Earth-Moon System
Sensitivity of the Asteroid Redirect Robotic Mission (ARRM) to Launch Date and Asteroid Stay Time
Acoustic Liner Design Utilizing Propagation Solvers of Varying Fidelity
Optimal orbits for sparse constellations of Mars navigation satellites
Mars, Phobos, and Deimos Sample Return Enabled by ARRM Alternative Trade Study Spacecraft
Simplified calculation of transition matrices for optimal navigation
Special orbits for the exploration of Mars and Venus
Evaluating the Performance of Hybrid Vehicles between LEO, Cislunar Space, and Mars
Optimum guidance for a low thrust interplanetary vehicle.