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Mode Projection Method for Target Mode Identification
Pterodactyl: Non-propulsive Control Systems for Future Planetary Missions
Human Mars Entry, Descent and Landing Architecture Study: Deployable Decelerators
Flutter Prediction for Aircraft Conceptual Design
Testing of the Lunar Reconnaissance Orbiter Attitude Control System Re-Design Without a Gyro
Sizing and Layout Design of an Aeroelastic Wingbox Through Nested Optimization
Contact with Bennu! Flight Performance Versus Prediction of OSIRIS-REx TAG Sample Collection
Pattern Recognition Control Design
Pattern Recognition Control Design
Nonlinear Analysis of a Two-Parachute System Undergoing Pendulum Motion
Interference Drag Associated with Engine Locations for Multidisciplinary Design Optimization
High Leverage Technologies for In-Space Assembly of Complex Structures
Three-Dimensional Modeling of Aircraft High-Lift Components with Vehicle Sketch Pad
Overview of the Transport Rotorcraft Airframe Crash Testbed (TRACT) Full Scale Crash Tests
Optimization of an Aeroservoelastic Wing with Distributed Multiple Control Surfaces
Assessment of Aeroacoustic Simulations of the High-Lift Common Research Model
Aeroservoelastic Optimization under Stochastic Gust Constraints
Emission Reduction with Heated Injectors
Parachute Models Used in the Mars Science Laboratory Entry, Descent, and Landing Simulation
Lessons Learned from Large-Scale Aerospace Structural Testing
A Simple Analytic Model for Estimating Mars Ascent Vehicle Mass and Performance
Development of an Integrated Data Acquisition System for a Small Flight Probe
Orion GN and C Model Based Development: Experience and Lessons Learned
Computational Aeroelastic Analyses of a Low-Boom Supersonic Configuration
Structures and Mechanisms Design Concepts for Adaptive Deployable Entry Placement Technology
Computational Optimization of a Natural Laminar Flow Experimental Wing Glove
Post-Flight EDL Entry Guidance Performance of the 2011 Mars Science Laboratory Mission
The Effect of Systematic Error in Forced Oscillation Testing
Aeroservoelastic Wind-Tunnel Test of the SUGAR Truss Braced Wing Wind-Tunnel Model
Orion Capsule Handling Qualities for Atmospheric Entry
Pattern Recognition for a Flight Dynamics Monte Carlo Simulation
A Flight Dynamics Model for a Multi-Actuated Flexible Rocket Vehicle
Analysis of Asymmetric Aircraft Aerodynamics Due to an Experimental Wing Glove
NASA/MOD Operations Impacts from Shuttle Program
Application of Adjoint Methodology in Various Aspects of Sonic Boom Design
The Sensor Test for Orion RelNav Risk Mitigation (STORRM) Development Test Objective
Seating Considerations for Spaceflight: The Human to Machine Interface
Crash Test of an MD-500 Helicopter with a Deployable Energy Absorber Concept
Aerostructural Level Set Topology Optimization for a Common Research Model Wing