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A Framework for Optimization-Based ISRU Tool Design Using Discrete Element Modeling
A space communication study Progress report, 15 Sep. 1966 - 15 Mar. 1967
Contensou-Busemann conditions for optimal coplanar orbit transfer.
Automatically Utilizing Science Opportunities with Continuous Plan Improvements
Ice Sheets System Model : Sensitivity Analysis : User Guide (Dakota)
Impact of Airspace Charges on Transatlantic Aircraft Trajectories
Rephasing and Loitering Strategies in the Gateway Near Rectilinear Halo Orbit
Thrust Direction Optimization: Satisfying Dawn's Attitude Agility Constraints
Rocket trajectory optimization final technical summary report, mar. 1961 - dec. 1964
Applications of the calculus of variations to aircraft performance
Design and Testing of the X-38 Spacecraft Primary Parafoil
Menagerie: an Automated Approach to Launch Vehicle Design
Design Optimisation and Mass Saving of the Structure of the Orion-MPCV European Service Module
Simplified calculation of transition matrices for optimal navigation
Optimal Integration of Departure and Arrivals in Terminal Airspace
Benefits Analysis of Wind-Optimal Operations For Trans-Atlantic Flights
A preliminary investigation of the Jupiter icy moon orbiter trajectory
A statistical optimization of the two-impulse transfer maneuver for a fixed-time rendezvous.
Identifying Accessible Near-Earth Objects for Crewed Missions with Solar Electric Propulsion
Identifying Accessible Near-Earth Objects For Crewed Missions With Solar Electric Propulsion
Minimum-fuel, two-impulse, soft lunar landing orbits
A direct and analytical solution for space flight guidance functions.
On the problem of comet orbit determination for spacecraft intercept missions
STUDIES IN THE FIELDS OF SPACE FLIGHT AND GUIDANCE THEORY. INTRODUCTION
Launch vehicle optimization, phase II. VOLUME I - Concept development and application Final report