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Stabilität
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keywords:(Stabilität)
Yaw rate control of an air bearing vehicle
X-48B Flight Research - Test Progress and Instrumentation Needs for the Future
X-38 Application of Dynamic Inversion Flight Control
X-33 Attitude Control Using the XRS-2200 Linear Aerospike Engine
X-33 Attitude Control System Design for Ascent, Transition, and Entry Flight Regimes
X-33 Ascent Flight Controller Design by Trajectory Linearization: A Singular Perturbational Approach
X-33 Ascent Flight Controller Design by Trajectory Linearization: A Singular Perturbational Approach
X-29A flight control system performance during flight test
Wing/store flutter with nonlinear pylon stiffness
Wing modification for increased spin resistance
Wing flap-type control effectiveness and effects of control hinge gap seals for a supercritical wing
Wind-Tunnel Tests of Hinge-Moment Characteristics of Spring-Tab Ailerons
WIND-TUNNEL TESTS OF A SERIES OF 18-FOOT-DIAMETER PARACHUTES WITH EXTENDABLE FLAPS
Wind-tunnel Tests of a Piston-type Control Booster on an Airfoil and Aileron Model
Wind-tunnel investigation of a Fowler flap and spoiler for an advanced general aviation wing
Wind tunnel investigation of active controls technology applied to a DC-10 derivative
Wind-tunnel investigation of a 1/20-scale powered model of a four-engine transport airplane