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A direct and analytical solution for space flight guidance functions.
Aeroelastic Tailoring Study of N+2 Low-Boom Supersonic Commercial Transport Aircraft
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.
A method of approximating propellant requirements of low-thrust trajectories
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
An Infeasible Interior-Point Arc-Search Algorithm for Spacecraft Trajectory Optimization
An Integrated Software Architecture for Solar Cruiser Mission Design and Navigation
An Optimized Trajectory for a Two-Stage, Surface-to-Orbit Titan Launch Vehicle
Applications of the calculus of variations to aircraft performance
A space communication study Progress report, 15 Sep. 1966 - 15 Mar. 1967
Assessment of Off-Design Low-Boom Characteristics of a Low-Boom Supersonic Transport
A statistical optimization of the two-impulse transfer maneuver for a fixed-time rendezvous.
Astrodynamics-optimization theory and guidance theory Research achievements review series no. 15-16
A structured approach to strategic decision making for NASA's technology development
Automated Multiple Maneuver Optimization (AMMO)
Automatically Utilizing Science Opportunities with Continuous Plan Improvements
Automatic design of optimum Atlas-Agena vehicle trajectories.
Benefits Analysis of Wind-Optimal Operations For Trans-Atlantic Flights
Blade and Trajectory Optimization of a Propeller-Driven Electric Aircraft with Acoustic Constraints
Building a pathway to Mars: Mars technology program analysis and case study
Challenges and Progress in Aerodynamic Design of Hybrid Wingbody Aircraft with Embedded Engines
Contensou-Busemann conditions for optimal coplanar orbit transfer.
Copernicus Spacecraft Trajectory Design and Optimization Program
Coupled Aeropropulsive Design Optimization of a Podded Electric Propulsor
Design and Testing of the X-38 Spacecraft Primary Parafoil