Speech recognition technology could be especially advantageous to single-crewmember helicopters like the Light Helicopter Family (LHX). Before speech recognition can be considered a viable technology for helicopters, several issues remain to be resolved. One of these is changes in the voice that occur as a result of stress, noise, and vibration. This paper reports the results of an investigation conducted to determine the effect of vibration-induced changes in the voice on the accuracy of a speech recognition system. A series of flight tests were conducted using 12 participants and 8 different flight maneuvers. Data were collected with the participants speaking 50 phonetically balanced words into the speech recognizer while seated in the copilot's seat of a UH-1H helicopter during each of the 8 flight maneuvers. The results indicate that speech recognition system accuracy is not affected by helicopter vibration.
Effect of Helicopter Vibration on the Accuracy of a Voice Recognition System
1986
15 pages
Report
Keine Angabe
Englisch
Verbal , Aircraft , Human Factors Engineering , Job Training & Career Development , Speech recognition , Voice communications , Helicopters , Vibration , Human factors engineering , Avionics , Flight crews , Stresses , Noise , Flight testing , Flight maneuvers , Phonetics , Voice recognition , UH-1H aircraft , H-1 aircraft
The effect of helicopter vibration on the accuracy of a voice recognition system
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|The effect of helicopter vibration on the accuracy of a voice recognition system
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