Objective Motion Cueing Criteria for Commercial Transport Simulators

Zaal, Petrus M ; Schroeder, Jeffery A ; Chung, William W

关键词: AIRLINE OPERATIONS;    COMMERCIAL AIRCRAFT;    CUES;    DEGREES OF FREEDOM;    ENGINE FAILURE;    PEDALS;    PILOT PERFORMANCE;    REACTION TIME;    SIMULATORS;    TAKEOFF;    TOUCHDOWN;    VERTICAL MOTION SIMULATORS;   

RP-ID  :  ARC-E-DAA-TN57232

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

This paper adds data to establish fidelity criteria for the simulator motion system diagnostic test now required during commercial aircraft simulator approval in the United States. Nineteen airline transport pilots flew three tasks under six different motion conditions in an experiment on the NASA Vertical Motion Simulator. The motion conditions allowed refinement of the initial fidelity criteria developed in previous experiments. In line with these previous experiments, the motion condition significantly affected (1) false motion cue pilot ratings, and sink rate and longitudinal deviation at touchdown in the approach and landing task, (2) false motion cue pilot ratings, roll deviations, and maximum pitch rate in the stall task, and (3) false motion cue pilot ratings, heading deviation, and pedal reaction time after an engine failure in the take-off task. Combining data from three experiments, significant differences in pilot-vehicle performance were used to define objective motion cueing criteria boundaries. These fidelity boundaries suggest that some hexapod simulators can possibly produce motion cues with improved fidelity in several degrees of freedom.