The pilot's perceptions of aircraft handling qualities are influenced by a combination of the aircraft dynamics, the task, and the environment under which the evaluation is performed. When the evaluation is performed in a groundbased simulator, the characteristics of the simulation facility also come into play. Two studies were conducted on NASA Ames Research Center's Vertical Motion Simulator to determine the effects of simulator characteristics on perceived handling qualities. Most evaluations were conducted with a baseline set of rotorcraft dynamics, using a simple transfer-function model of an uncoupled helicopter, under different conditions of visual time delays and motion command washout filters. Differences in pilot opinion were found as the visual and motion parameters were changed, reflecting a change in the pilots' perceptions of handling qualities, rather than changes in the aircraft model itself. The results indicate a need for tailoring the motion washout dynamics to suit the task. Visual-delay data are inconclusive but suggest that it may be better to allow some time delay in the visual path to minimize the mismatch between visual and motion, rather than eliminate the visual delay entirely through lead compensation.
Effects of Simulator Motion and Visual Characteristics on Rotorcraft Handling Qualities Evaluations
1993
19 pages
Report
No indication
English
Aircraft , Aeronautics , Test Facilities & Equipment , Human Factors Engineering , Flight characteristics , Flight simulators , Helicopter performance , Rotary wing aircraft , Vertical motion simulators , Visual fields , Controllability , Flight simulation , Helicopter control , Aircraft models , Evaluation , Time lag , Transfer functions
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