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50-percent change aerodynamic aileron deflection angle aircraft mode angle of attack automatic reentry flight block diagram body axis body flap CD Q CD T CD CD W H center-of-gravity Chord commanded aileron circuit control hysteresis producing CONTROL SYSTEM FUEL deg kg due to aileron dynamic pressure Effects of Control equivalent aileron deflection error signal Figure flight control system flight dynamics simulator GUIDANCE SAMPLING guidance system hysteresis was modeled Langley Research Center Lawrence F little increase Master of Science model with remotely NASA NASA Langley Research NASA TM nominal value oscillation payload Performing Organization pitching-moment Powell rate about body RCS fuel reaction control system reentry flight dynamics Reference area remotely controlled elevons rolling moment due rudder sampling frequencies sec from deorbit shuttle orbiter entry shuttle orbiter model space shuttle orbiter spacecraft mode SYSTEM FUEL CONSUMPTION tolerate control hysteresis trol hysteresis turn coordination Wind-tunnel wing yaw thrusters