A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY
UNMANNED AERIAL VEHICLE — HUMAN PERFORMANCE EVALUATION UNDER CRITICAL OPERATIONAL SCENARIO
An Approach for Automation the Satellite of Routine's Operation and Procedures (AIAA 2014-1846)
Active Reduction of Common Mode Current in Power Modules
Airbreathing Hypersonic Laser Thermal Propulsion Experiments with a LightCraft Vehicle-Status Update
High Order Weighted Compact Scheme for Shock/Boundary Layer Interaction
Verification and Validation of LES for Interaction of Wingtip Vortex and Wakes
ON THE CORRELATION OF ACOUSTIC MODES IN A NOZZLE AND IN THE FAR-FIELD
Development of Surface Junction Thermocouples for High Enthalpy Measurements
Mapping Brazil with Advanced Land Observing Satellite (ALOS)
Oceanographic Characterization of the Cape Verde Region Using Multisensor Data (332)
Flow Visualization of Laser-Induced Air Spikes in Hypersonic Flow
ON SOUND ATTENUATION IN A NOZZLE WITH NON-UNIFORM LINING
Multi Laser Pulse Investigation of the DEAS Concept in Hypersonic Flow
A Semi-Analytical Method to Generate Load Cases for CAE Durability Using Virtual Vehicle Prototypes
Forming Analysis Results Influences on Safety Crash Finite-Element Analyses
The Development of a New Tailcone for a Regional Aircraft: A Multidisciplinary Approach
The Development of a New Tailcone for a Regional Aircraft: A Multidisciplinary Approach
Feature Sets Evaluation for Handwritten Word Recognition
2001-01-0824 Simulation of Electromagnetic Forming of Aluminum Alloy Sheet
Preliminary Investigation of Circumstellar Emission and Flares in the Fast Rotating Giant FK Comae
Working conditions of Brazilian flight attendants: A qualitative approach
Preliminary MUSICOS 96 Results on Balmer Line Variability on the T Taura Star SU Aurigae
An Efficient Algorithm for Infinite-Norm Robust Predictive Controller with Guaranteed Stability
Soliton propagation in the vicinity of a two-photon resonance
Experimental study of color control on reflection holography [3011-26]
On Sound Transmission through Boundary Layers of Aircraft Fuselages and Engine Ducts
On the Acoustics and Stability of Low- and High-Speed Shear Flows