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88269 Model-Following Control advantage for aircraft aerodynamic and inertial aerodynamic performance advantage Aerospace Engineer aileron command aircraft longitudinal aircraft missions Alag Ames Research Center Angle of attack ApXp associated with wing-skew asymmetry associated bank angle 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 equations of motion equations of six explicit model following Febo Bartoli feedforward flight and supersonic flight condition Flight Research Facility freedom of motion I I I I I I I I I I inertial cross-coupling Kempel missions that require model response Model-Foll owing Systems model-following control law NASA Ames Research nonlinear equations o.ooo oblique wing offers oblique-wing concept optimal control optimization OWRA Pahle Performing Organization Pitch rate require both high Research Center Dryden simulation six degrees stability and decoupling subsonic flight supersonic dash yaw rate