A direct and analytical solution for space flight guidance functions.
Aeroelastic Tailoring Study of N+2 Low Boom Supersonic Commerical Transport Aircraft
A Framework for Optimization-Based ISRU Tool Design Using Discrete Element Modeling
A general method for determining optimum thrust nozzle contours for gas-particle flows.
A History of Orion Mission Design, Copernicus Software Development, and the Artemis I Trajectory
A manual optimal guidance scheme using a predictive model.
Analysis of Near Rectilinear Halo Orbit Insertion with a 40-kW Solar Electric Propulsion System
A New Eclipse Algorithm for use in Spacecraft Trajectory Optimization
A New Mission Concept for the Space Infrared Telescope Facility
An Integrated Software Architecture for Solar Cruiser Mission Design and Navigation
A preliminary investigation of the Jupiter icy moon orbiter trajectory