A Robust Design Method for Direct MRAC System in the Presence of Disturbances
Discrete-Time Robust Adaptive Control of an Uncertain Plant with Delay
A model vehicle with magnetic flux pinning effects of high-Tc oxide superconductors
TuC2 TN and GH-LCDs fabricated by non-rubbing techniques and an overview of LCDs in Japan
Development of Rolling Stock Reliability Analysis System
Postflight Evaluation of the HYFLEX Guidance, Navigation, and Control
Flight Control Design of Hypersonic Flight Experiment (HYFLEX) Vehicle
EPEX Flight Test Onboard SFU-1 - Thruster, Propellant Supply System and Thermal Control System-
Analysis of Body Temperature Distributions Generated by an Ultrashortwave Apparatus
Flight Data Analysis for the Integrated Navigation of ALFLEX (Automatic Landing Flight Experiment)
Neoplastic Transformation of Hamster Embryo Cells by Heavy Ions
Fault Diagnosis of Space Vehicle Guidance and Control Systems using Analytical Redundancy
Development of a New Electronically Controlled 4WD System: Toyota Active Torque Control 4WD
Influence of Double Image on the Troublesomeness of a Head-Up Display for Use in Motor Vehicles
Fault Diagnosis of Space Vehicle Guidance and Control Systems Using Analytical Redundancy
Thrust Performance and Thermal Analysis of a Low Power Arcjet Thruster
Inquiry into Radio Noise Conditions on the Real Road
Effect of start of injection on NOx and smoke emissions in homogeneous charge diesel combustion
Real-time recognition of corridor under varying lighting conditions for autonomous vehicle
Real-time recognition of Corridor under Varying Lighting Conditions for Autonomous Vehicle
Real-time Visual Recognition by Autonomous Vehicle for Intelligent Transportation System
Guidance and Control Design for HOPE-X High Speed Flight Demonstrator Phase II
Current-Sheet Kink Instability at Ion-Electron Hybrid Scale
2003-01-0817 Development of PZEV Exhaust Emission Control System
Mixture Formation and Auto-Ignition Behavior of Pure and Mixed Normal Paraffin Fuels
AIAA-2004-4944 Guidance and Control for the High Speed Flight Demonstration: Phase II
Space Demonstration of a Fault Tolerant Computer System using Commercial MPU