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Stabilität
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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 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