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Aircraft
•
Stability
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keywords:(Aircraft Stability and 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
WIND-TUNNEL TESTS OF A SERIES OF 18-FOOT-DIAMETER PARACHUTES WITH EXTENDABLE FLAPS
Wind Tunnel Testing Techniques for a Tandem Tilt-Wing, Distributed Electric Propulsion VTOL Aircraft
Wind Tunnel Testing of the NASA-DFRC Flutterometer using a Two DOF Wing Section
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