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Simulator Evaluation of a Flight-Path-Angle Control System for a Transport Airplane With Direct Lift Control

机译:直升机控制的运输机飞行路径角控制系统仿真评估

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A piloted simulator was used to evaluate the flight-path-angle control capabilities of a system that employs spoiler direct lift control. This system was designated the Velocity Vector Control System and was compared with a baseline flight-path-angle control system which used elevator for control. The simulated airplane was a medium jet transport that is used as a research vehicle by the National Aeronautics and Space Administration (NASA). Research pilots flew a manual instrument landing system glide-slope tracking task and a variable flight-path-angle task in the landing configuration to obtain comparative performance data.

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