## Moving-base Visual Simulation Study of Decoupled Controls During Approach and Landing of a STOL Transport Aircraft |

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70 knots aerodynamic aircraft response airplane angle of attack appendix approach and landing Blown Flap closed-circuit television coefficient COMPUTED FLIGHT DATA constant prefilter constant-speed two-segment approach control gains damping ratio DATA WASHOUT DATA decoupled longitudinal controls deflection degrees of freedom degrees or radians desired glide slope ENGINE RESPONSE CHARACTERISTICS equations of motion externally blown Figure 12 fixed-base simulation flap FLIGHT DATA WASHOUT flight director flight-path angle forward velocity g units gain matrix given a pilot ground effect intensity of 0.3 lateral mode longitudinal mode low-level turbulence m/sec 2 ft/sec meters ft moving-base simulator NASA TN nondimensional optimal control p0r d0g performance index phugoid pilot believed pilot compensation pilot rating pitch angle prefilter and feedback prefilter gain presented in figure presented in table rad/sec rate and sideslip research pilot Riccati equation sec Figure set of gains sideslip angle sink rate STOLport Turbulence level U.S. Customary Units vector