AIAA-2003-6798 Airship Shaped Balloon Test Flights to the Stratosphere
Assessment of SAR Ocean Features Using Optical and Marine Survey Data
Specialized Ship Mooring Problems: Transient Loadings and Long Period Waves
Light Rail in Britain and France: Study in Contrasts, with Some Similarities
Comparison of Supportability Analysis Techniques for Lunar Surface Systems Elements
AIAA-2006-1805 Measurement of In-Plane Motion of Thin-Film Structures Using Videogrammetry
Mach 10 Boundary Layer Transition Experiments on Sharp and Blunted Cones (Invited) (AIAA 2014-3108)
Parametric Study of the Effect of Membrane Tension on Sunshield Dynamics
Drag and Steering Effects from Tire Tread Belt Separation and Loss
Performance Assessment of the EOS Space Debris Tracking System
AIAA-2004-4968 Active Multiple Winglets for Improved UAV Performance
Combined Aerospace Testing: Bridging the Gap Between Airborne and Space Systems
Model-Based Diagnostic Approach to Acquisition in a System-of-Systems Context
Progress in Automated Ground Control of ESA's Gaia Mission (AIAA 2018-2603)
Interface Control-The Secret to Making DFMA[R] Succeed
Real Time Tracking of Geostationary Satellites in Sub Arc Second Accuracy
2007 01 1181 Restraint Robustness in Frontal Crashes
STREAM FUNCTION CALCULATION ON GENERAL SURFACE MESH TOPOLOGIES AND GENERAL GEOMETRIES
Determination of On-Orbit Cabin Air Loss from the International Space Station (ISS)
Measurement and Simulation of Sl Engine Fire-Up on hydrogen Fuel
Gyroscopic data fusion via a quaternion-based complementary filter [3067-08]
General Aviation Collision Avoidance-Challenges of Full Implementation
A Preliminary Design Study of a Joint Primary Aircraft Trainer (JPAT)
AIAA-2006-6767 Designing On-Demand Coded Departure Routes
Improvements in the Computational Modeling of Rotor/Fuselage Interactions Using Unstructured Grids
Effects of Automated Arrival Management, Airbone Spacing, Controller Tools, and Data Link AIAA Paper
Affordable Nacelle Technologies for Future Turbofans
Affordable Nacelle Technologies for Future Turbofans
Near Real Time Global Lake and River Monitoring Using the Envisat RA-2
NEXT GENERATION CONTROL SYSTEM FOR HELICOPTER ENGINES
Fixed Format Liquid Crystal Display Readability in Bright Ambient Environments
Refinements to the Aerodynamic Modeling of an Ascending Balloon