Integrated approach to an optimal automotive timing chain system design
AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING
Bacteriophages as Templates for Manufacturing Supramolecular Structures
FDI for Intertial Sensor using Single Antenna GPS Receiver
Running Model for a Compliant Wheel-Leg Hybrid Mobile Robot by Using a Mass-Spring Model
Structure of Compression Waves on Supersonic Droplets
Structure of Compression Waves on Supersonic Droplets
A New BDT-Based Conjugated Polymer with Donor-Donor Composition for Bulk Heterojunction Solar Cells
ON SATELLITE ATTITUDE CAPTURING BY THE GRAVITY GRADIENT TORQUE CONDITION AND PASSIVE SAFE HOLD MODE
Vehicle's Model Classification Using a Vertical Stereo Camera
IS17-38 Hybrid Fault Detection and Isolation of UAV Sensor System
Dynamic Modulus Testing of Asphalt Concrete in Indirect Tension Mode
Dual-Probe Linearly Configured BOCDA System With Enlarged Modulation Amplitude
Simple and Effective Modelling Technique of Exhaust System
Incremental Model for Prediction of Permanent Deformation of Asphalt Concrete in Compression
Experimental Investigation of Anisotropy in Asphalt Concrete
Experimental Investigation of Anisotropy in Asphalt Concrete
A Note on Edge-based Graph Partitioning and its Linear Algebraic Structure
A Development of a Transonic Mixed-Flow Compressor for UAV Applications
A Study on the Low-Weight BMC for Headlamp Reflector
Design of Reconfigurable Flight Control System Using Adaptive Sliding Mode Control: Actuator Fault
Design of reconfigurable flight control system using adaptive sliding mode control: actuator fault
On-Line Traffic Flow Model Applying The Dynamic Flow-Density Relation
Development of a Parallel-Type Diesel Hybrid Bus and Fuel Efficiency Results from Trial Runs
Predicting the Resilient Modulus of Asphalt Concrete from the Dynamic Modulus
New algorithm and accelerometer locations for frontal crash discrimination
New algorithm and accelerometer locations for frontal crash discrimination
AIAA-2004-5420 Variable Structure Control with Optimized Sliding Surface for Aircraft Control System