Adjoint-based Shape and Kinematics Optimization of Flapping Wing Propulsive Efficiency
A Feasibility Study of the Use of Axisymmetric Thrust Vectoring for Enhanced In-Flight Simulation
AIAA 2006-1309 Azimuthal Vorticity Dynamics and Vortex Breakdown Above a Delta Wing
AIAA-2006-6084 A New Off-Axis Laser Beamrider Missile Guidance Algorithm
An Object-Oriented Mission Control System Development: Report on SCOS-II
A Quasi-3-D Theory for Impedance Eduction in Uniform Grazing Flow AIAA Paper 2005-2848
A Special Oil Recovery Tug: The SORT 33 - A New Tug with a Mission
Comparison of RVR System Estimates and Human Observations Under Category IIIb Conditions
Comparison of Simulator Platform and Flight Tasks on Adverse Rotorcraft Pilot Coupling Prediction
Cost Reduction Through Application of Fieldbus Technology to Space Mission Operation and Control
Design for Assembly - A Strategy for Right First Time Design
Detecting Pedestrians Using Patterns of Motion and Appearance
Development of a Low-Emission, Dedicated Ethanol-Fuel Vehicle with Cold-Start Distillation System
Dynamics of the Vortex Core During Pitching of a High-Sweep Delta Wing AIAA Paper
ESA Software Engineering Standards and ISO 9001: Theory and Practice