Recognizing objects in adversarial clutter: breaking a visual CAPTCHA
Recognizing Objects in Adversarial Clutter: Breaking a Visual CAPTCHA
Planning the Oakland Airport Connector Alignment to Enhance Passenger Service
Planning the Oakland Airport Connector Alignment to Enhance Passenger Service
A New Attitude Maneuver Using Kinematics and Dynamics of Non-Holonomic Turn (AAS 06-100)
Shape contexts enable efficient retrieval of similar shapes
Shape Contexts Enable Efficient Retrieval of Similar Shapes
Development of Gas-Liquid Equilibrium Thruster for the Small Satellite
INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS
Recovering human body configurations: combining segmentation and recognition
Recovering Human Body Configurations: Combining Segmentation and Recognition
Design of Kurushima Bridge: Aesthetics and aerodynamics
CsLiB~6O~1~0 crystal: growth and properties (Invited Paper) [2700-02]
Control of Launch Vehicles as Flexible Bodies
Strategic Project Optimizing Advice for the Miami International Airport Connector
Analysis of photon-number squeezed light generation using nonlinear polarization interferometer
Analysis of Photon-Number Squeezed Light Generation Using Nonlinear Polarization Interferometer
Solar and Thermal Radiation Pressure Models and Flight Evaluation for Ikaros Solar Sail (AAS 14-244)
Improved Heat Resistant Acrylic Rubber for Engine Oil Seals
Mission Analysis of Near Earth Asteroid Exploration by Miniature Asteroid Interceptors (AAS 06-212)
Precise surface measurement by local sampling phase-shifting technique [2860-14]
IKAROS, a Solar Sail Demonstrator and Its Application to Trojan Asteroid Exploration
A Study on Membrane Deformation of Solar Power Sail Demonstrator IKAROS
A Novel Intelligent IGBT with Constant Current Limiting Circuit for Automotive Ignition Application
System Analysis and Trajectory Optimization of an Ejector-Ramjet Powered Reusable Launch Vehicle
Deployment Experiment of Thin Flexible Membrane Using Sounding Rocket for Future Solar Sail Mission
System Concept of the Mid-term Target RLV- Reusable Booster Returned by Ramjet Cruising Propulsion -
On Single-Wheel Configured Spacecraft and the Attitude Stability Revisited (AAS 08-139)