Execution of environmental protecting measures at Motosumiyoshi Station of Toyoko Line
Recognizing Objects in Adversarial Clutter: Breaking a Visual CAPTCHA
A New Attitude Maneuver Using Kinematics and Dynamics of Non-Holonomic Turn (AAS 06-100)
Development of Gas-Liquid Equilibrium Thruster for the Small Satellite
INTEGRATED UAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS
Shape Contexts Enable Efficient Retrieval of Similar Shapes
CsLiB~6O~1~0 crystal: growth and properties (Invited Paper) [2700-02]
Design of Kurushima Bridge: Aesthetics and aerodynamics
Control of Launch Vehicles as Flexible Bodies
Strategic Project Optimizing Advice for the Miami International Airport Connector
Recovering Human Body Configurations: Combining Segmentation and Recognition
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
Precise surface measurement by local sampling phase-shifting technique [2860-14]
Mission Analysis of Near Earth Asteroid Exploration by Miniature Asteroid Interceptors (AAS 06-212)
Amphiphilic Poly(N-propargylamide) with Galactose and Lauryloyl Groups: Synthesis and Properties
Analysis of Photon-Number Squeezed Light Generation Using Nonlinear Polarization Interferometer
IKAROS, a Solar Sail Demonstrator and Its Application to Trojan Asteroid Exploration
Planning the Oakland Airport Connector Alignment to Enhance Passenger Service
Development of Mitsubishi single point mooring (SPM) system for open sea operation
Development of automatic control system and diagnostic system for a mini-tunnel
System Analysis and Trajectory Optimization of an Ejector-Ramjet Powered Reusable Launch Vehicle
A Novel Intelligent IGBT with Constant Current Limiting Circuit for Automotive Ignition Application
A Study on Membrane Deformation of Solar Power Sail Demonstrator IKAROS
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)
Development of a Large Torque Capacity Half-Toroidal CVT
Dynamic and Static Deployment Motions of Spin Type Solar Sail
Ultra-Capacitor and Battery Hybrid EV with High Efficiency Battery Load Leveling System