A vibrotactile system for an aircraft may comprise a plurality of tactors and a tactor driver operably coupled to the plurality of tactors. The tactor driver may be configured to determine a vibration sequence for the plurality of tactors in response to a signal received from an aircraft controller, and to send vibration commands corresponding to the vibration sequence to the plurality of tactors.
Vibrotactile systems and methods for aircraft seats
2025-01-28
Patent
Electronic Resource
English
VIBROTACTILE SYSTEMS FOR AIRCRAFT, METHODS FOR OPERATING THE SAME, AND EJECTION SEATS
European Patent Office | 2023
|Engineering Index Backfile | 1950
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