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Energy-Based Design of Reconfigurable Micro Air Vehicle (MAV) Flight Structures
Design of Airframe-Integrated, Distortion-Tolerant Propulsion Systems
Guidance, Flight Mechanics and Trajectory Optimization. Volume 13 - Numerical Optimization Methods
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
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
Flight Dynamics: Trajectories of Flight Vehicles (Selected Parts)
Simulation Optimization Approach to the Design of Unmanned Aerial Vehicles
Design Optimization of a Variable-Speed Power Turbine
Flexible Wing Designs with Sensor Control Feedback for Demonstration on the X-56A (MUTT)
Hybrid Wing Body Planform Design with Vehicle Sketch Pad
Investigation of Abort Procedures for Space Shuttle-Type Vehicles
Features of the Process of Optimization of High Speed Soaring Flight
Flight Optimization System Weights Estimation Method
Conceptual Design: Optimization of Medium Scale Unmanned Aerial Vehicle Propulsion System
COTSAT Small Spacecraft Cost Optimization for Government and Commercial Use
ARC Accomplishments and Collaborations Pursuing Challenges with Vision and Focus
Global Optimization of Low-Thrust Interplanetary Trajectories Subject to Operational Constraints
Aerodynamic Limits on Large Civil Tiltrotor Sizing and Efficiency
Reduction Method with System Analysis for Multiobjective Optimization-Based Design
Optimization of the Time Between Aircraft Overhauls by Minimizing Maintenance Cost
Integral Launch and Reentry Vehicle System. Volume 4 - One and a Half Stage Configuration