Publication Date:
2019-06-28
Description:
A moving-base simulation was conducted to investigate a pilot's ability to recover from transients following single-axis hard-over failures of the flight-control system. The investigation was performed in conjunction with a host simulation that examined the influence of control modes on a single pilot's ability to perform various mission elements under high-workload conditions. The NASA Ames large-amplitude-motion Vertical Motion Simulator (VMS) was utilized, and the experimental variables were the failure axis, the severity of the failure, and the airspeed at which the failure occurred. Other factors, such as pilot workload and terrain and obstacle proximity at the time of failure, were kept as constant as possible within the framework of the host simulation task scenarios. No explicit failure warnings were presented to the pilot. Data from the experiment are shown, and pilot ratings are compared with the proposed handling-qualities requirements for military rotorcraft. Results indicate that the current proposed failure transient requirements may need revision.
Keywords:
AIRCRAFT STABILITY AND CONTROL
Type:
NASA-TM-100078
,
A-88113
,
USAAVSCOM-TM-88-A-001
,
NAS 1.15:100078
,
AD-A198150
,
ARC-E-DAA-TN10470
Format:
application/pdf
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