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Aviation Weather Routing Tool: A Decision Aid for Manned/Unmanned Aircraft Routing
Energy-Based Design of Reconfigurable Micro Air Vehicle (MAV) Flight Structures
Guidance, Flight Mechanics and Trajectory Optimization. Volume 13 - Numerical Optimization Methods
Design of Airframe-Integrated, Distortion-Tolerant Propulsion Systems
Review of X-33 Hypersonic Aerodynamic and Aerothermodynamic Development
Basis Function Approximation of Transonic Aerodynamic Influence Coefficient Matrix
Basis Function Approximation of Transonic Aerodynamic Influence Coefficient Matrix
Further Development of the NASA X-57 Maxwell Mission Planning Tool for Mods II, III, and IV
Deconflicting Wind-Optimal Aircraft Trajectories in North Atlantic Oceanic Airspace
Automated Method to Compute Orbital Re-entry Trajectories with Heating Constraints
Automated Method to Compute Orbital Re-Entry Trajectories with Heating Constraints
Flight Dynamics: Trajectories of Flight Vehicles (Selected Parts)
Simulation Optimization Approach to the Design of Unmanned Aerial Vehicles
Optimized Algorithms for Prediction Within Robotic Tele-Operative Interfaces
Error Analysis and Performance Optimization of Rocket Vehicle Guidance Systems
Optimum Motion in a Central Field when the Operation Time of a Propulsion System Is Given
Flexible Wing Designs with Sensor Control Feedback for Demonstration on the X-56A (MUTT)
Hybrid Wing Body Planform Design with Vehicle Sketch Pad
Features of the Process of Optimization of High Speed Soaring Flight
Conceptual Design: Optimization of Medium Scale Unmanned Aerial Vehicle Propulsion System
COTSAT Small Spacecraft Cost Optimization for Government and Commercial Use
Investigation of Abort Procedures for Space Shuttle-Type Vehicles
ARC Accomplishments and Collaborations Pursuing Challenges with Vision and Focus
Interaction of strategic defenses with crisis stability. Part 3, Summary and conclusions
Global Optimization of Low-Thrust Interplanetary Trajectories Subject to Operational Constraints
Aerodynamic Limits on Large Civil Tiltrotor Sizing and Efficiency
Integral Launch and Reentry Vehicle System. Volume 4 - One and a Half Stage Configuration
Reduction Method with System Analysis for Multiobjective Optimization-Based Design
Optimization of the Time Between Aircraft Overhauls by Minimizing Maintenance Cost