Structural Optimization of Joined-Wing Beam Model with Bend/Twist Coupling Using ESL
Finite Element Model Tuning with 3D Mode Shapes from FalconSAT-5
Rigidizable Inflatable Get-Away-Special Experiment (RIGEX) Space Flight Data Analysis
A Persistent Monitoring System to Reduce Navy Aircraft Carrier Flight Deck Mishaps
2001-01-2770 System Requirements for the Electronics Integration Test Station
2001-01-2769 Electronics Integration Test Station Development Methods
AIAA-2006-2236 Efficient Frequency Response Analysis of Structures with Viscoelastic Materials
Hardware Testing of Hybrid Steering Logic for Single-Gimbal Control Moment Gyroscopes
Uncertainty Modeling and Identification from GVT Test Data
Near Real-Time Closed-Loop Optimal Control Feedback for Spacecraft Attitude Maneuvers
Follower-Force Experiments with Geometric Nonlinear Coupling for Analytical Validation
Development and Design of an AFIT CubeSat Demonstrating Deployable Technology
Experiments with Geometric Non-Linear Coupling for Analytical Validation
Prototype Development and Dynamic Characterization of Deployable CubeSat Booms
Aeroelastic Analysis and Optimization of FalconLAUNCH Sounding Rocket Fins