Current Airspace Configuration Practices and Their Implications for Future Airspace Concepts
Cost-Benefit Analysis on Deployment of Automated Highway Systems
Conformance Monitoring under Uncertainty in Trajectory
Conditions of Frictional Contact in Disk Brakes and their Effects on Brake Judder
Computational Prediction and Comparison of Ground versus Air Launced Rocket Noise AIAA Paper
Characterization of OPCPA with BBO crystal for femtosecond Ti:sapphire laser pulses
Brake Thermal Analysis with Additional Consideration (20025319)
AVEC060225 Development of Integrated Chassis Control Algorithms to Improve Vehicle Dynamics
Automatic coding of facial expressions displayed during posed and genuine pain
ATTRACTIVE MANIFOLD-BASED NONCERTAINTY-EQUIVALENT ADAPTIVE CONTROL OF AIRCRAFT
A Study on the Vehicle Dynamics Properties using Active Roll Control Stabilizer Bar System
A study on recognition of lane and movement of vehicles for port AGV vision system
A Study of Nano-particle Characteristics of After-treatment System for a Heavy Duty Diesel Engine
Application of Complexity Map to Reduce Air Traffic Complexity in a Sector (AIAA 2014-1461)
An investigation of optimal fuel injection conditions for the reduction in hydrocarbon emission
An Analytical Method to Predict Thermal Distortion of a Brake Rotor
Analysis of Gossamer Structures Using Assumed-Strain Solid-Shell Finite Elements
Analysis of Gossamer Space Structures Using Assumed Strain Formulation Solid Shell Elements
Analysis of dynamic contact between overhead wire and pantograph of a high-speed electric train
AIAA-2006-6315 Global Robust Control of Aeroelastic System Using Output Feedback
AIAA 2006-1517 Breakup of Turbulent and Non-Turbulent Liquid Jets in Gaseous Crossflows
AIAA-2002-5485 Reliability Based Shape Optimization of a Funnel in Cathode Ray Tubes
A Grinding Machine Spindle With Capacitance Type Gap Sensor Supported By Hydrostatic Journal Bearing
Aerodynamic Model Reconstruction via Probabilistic Principal Component Analysis
Adaptive Output Feedback Spacecraft Formation Flying Via Observer Based Feedback Linearization
Adaptive Control of Spacecraft with Flexible Appendages Using Nussbaum Gain AIAA Paper