Worldwide Mission Planning Tool for Tactical Laser Systems
Work Models that Compute to Describe Multiagent Concepts of Operation: Part 1
Wing Kinematics Optimization for Hovering Micro Air Vehicles Using Calculus of Variation
Wind-Tunnel Testing of Otto Lilienthal’s Production Aircraft from 1893
Wind-Tunnel Study of Gurney Flaps Applied to Micro Aerial Vehicle Wing
Wind Tunnel Experiment of Microjet-Based Flow Control on a Two-Dimensional Wing with Flap
Wide-Ranging Viscosity Measurements of Rocket Propellant RP-2
Wedge-Induced Oblique Detonations with Small Heat Release
Wave Mode Dynamics in an Ethylene-Air Rotating Detonation Combustor
Water-Treading Motion for Three-Dimensional Flapping Wings in Hover
Vortex Shedding and Aerodynamic Performance of Airfoil with Multiscale Trailing-Edge Modifications
Visual Perception-Based Target Aircraft Movement Prediction for Autonomous Air Combat
Vision-Based Landing of Fixed-Wing Miniature Air Vehicles
Vision-Based Cyclic Pursuit for Cooperative Target Tracking
Virtual Simulation-Based Evaluation of Ground Handling for Future Aircraft Concepts
View Invariants for Three-Dimensional Points with Constrained Observer Motion
Vertical State Estimation for Aircraft Collision Avoidance with Quantized Measurements
Vertically Optimal Close Formation Flight Control Based on Wingtip Vortex Structure