Model-following Control for an Oblique-wing Aircraft1986 - 13 pages |
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advantage for aircraft aerodynamic and inertial aerodynamic performance advantage Aerospace Engineer AIAA aileron command input aircraft longitudinal aircraft missions Alag Ames Research Center Angle of attack Apxp associated with wing-skew asymmetry associated Bmum Bpup Bresina Center Dryden Flight control laws developed control theory dash or cruise Decoupling Control deg/sec degrees of freedom desired stability augmentation Dryden Flight Research dynamics elevator command input equations of motion equations of six explicit model following Febo Bartoli flight and supersonic Flight Research Facility freedom of motion inertial cross-coupling Joseph W Kempel linear feedback system missions that require Model Aircraft model fol model response model-following control law NASA NASA Ames Research nonlinear equations oblique wing offers oblique-wing concept optimal control OWRA Pahle pitch angle Pitch rate require both high Research Center Dryden response to aileron response to elevator simulation six degrees stabilization and decoupling subsonic flight supersonic dash wing-skew angle Yaw rate