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HELICOPTERS
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keywords:(HELICOPTERS)
Vortex Particle Method Whirl-Flutter Predictions of a Tiltrotor with Wing Extensions
Vortex modeling for rotor- aerodynamics - The 1991 Alexander A. Nikolsky Lecture
Vortex Model and Blade Span Influence on Orthogonal Blade-Vortex Interaction Noise
Vortex methods for the computational analysis of rotor/body interaction
Vortex Methods for the Computational Analysis of Rotor-Body Interaction
Vortex cutting by a blade, Part 1: General theory and a simple solution
Vortac Error Analysis for Helicopter Navigation; New York City Area
V Krajowe Forum Wiropłatowe : [Warszawa, 17 - 18.10.2003]
Visual Workload of the Copilot/Navigator During Terrain Flight
Visual servoing of an under-actuated dynamic rigid-body system: an image-based approach
Visual Sensitivities and Discriminations and Their Roles in Aviation
Visual Problems and Night Landing Guidance of the CH-47 (Chinook) Helicopter
Visual Performance/Workload of Helicopter Pilots during Instrument Flight
Visual Meteorological Conditions (VMC) Right Turn Curved Approaches
Visual control of an unmanned aerial vehicle for power line inspection
Visual Augmentation System (VAS) Laboratory Demonstration and Test Results
Visit to SIAI-Marchetti, Sesto-Calende/Vergiate (Varese), Italy
Vision based techniques for rotorcraft low altitude flight
Vision-based target recognition and autonomous flights through obstacle arches with a small UAV
Vision-based servo control of a quadrotor air vehicle
Vision-based fuzzy 2D motion control of a model helicopter
VISION-BASED DECK STATE ESTIMATION FOR AUTONOMOUS SHIP-BOARD LANDING
Vision-based autonomous navigation and landing of an unmanned aerial vehicle using natural landmarks
Vision-augmented inertial navigation by sensor fusion for an autonomous rotorcraft vehicle
Vision and courage in helicopter design
Viscous Flow Simulation of Rotor Blades with Tip Slots in Hover
Viper CNC fibre placement system for tiltrotor aircraft
Videogrammetric system for studying movement and deformation of real-scaled helicopter rotor blades
Vibratory Loads Reduction Testing of te NASA-Army-MIT Active Twist Rotor
Vibratory Loads Data from a Wind-Tunnel Test of Structurally Tailored Model Helicopter Rotors
Vibrations of helicopter rotor-fuselage system induced by main rotor blades in flight