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- W2332856816 abstract "Tests performed on a 6 degrees-of-freedom flight simulator with pilots at two extreme levels of alertness were used to define parameters based on aircraft states and pilot input measurements that can serve as pilot fatigue on-line detectors. These parameters were computed using the statistics of the tracking errors, state and control time histories, and the Fourier transforms of the tracking errors. Based on the analysis of the performance of candidate detectors at steady state flight conditions, composite parameters were defined and implemented within an on-line pilot fatigue detection scheme. The design of the proposed pilot fatigue detection algorithm applies to steady state flight conditions and assumes the availability of on-board aircraft state and pilot input measurements. Validation tests on the flight simulator showed that the proposed detection scheme - as an alternative to approaches based on physiological measurements - has promising capabilities for safety monitoring purposes and design of control laws that can accommodate for pilot abnormal conditions." @default.
- W2332856816 created "2016-06-24" @default.
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- W2332856816 date "2008-06-15" @default.
- W2332856816 modified "2023-09-27" @default.
- W2332856816 title "Development of Pilot Fatigue Detection Schemes Based on Aircraft Sensor Measurements" @default.
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- W2332856816 doi "https://doi.org/10.2514/6.2008-7111" @default.
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