An analytical and experimental study of the human pilot control strategies in a manned rotorcraft simulation is described. The task simulated involves a low-speed, constant-altitude maneuvering task in which a head-down display is utilized to allow the pilot to track a moving hover point. The efficacy of the display law driving an acceleration symbol is determined and the manner in which the prediction and measurement of pilot/vehicle dynamics can be made part of man/machine system evaluations is demonstrated.
Prediction and Measurement of Human Pilot Dynamic Characteristics in a Manned Rotorcraft Simulation
1988
44 pages
Report
No indication
English
An Aeroelastic Model Structure Investigation for a Manned Real-Time Rotorcraft Simulation
British Library Conference Proceedings | 1993
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