A vibrotactile system for an aircraft may comprise a plurality of tactors (122, 124) and a tactor driver (130) operably coupled to the plurality of tactors (122, 124). The tactor driver (130) may be configured to determine a vibration sequence for the plurality of tactors (122, 124) 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 (122, 124).
VIBROTACTILE SYSTEMS AND METHODS FOR AIRCRAFT SEATS
VIBROTAKTILE SYSTEME UND VERFAHREN FÜR FLUGZEUGSITZE
SYSTÈMES VIBROTACTILES ET PROCÉDÉS POUR SIÈGES D'AVION
20.12.2023
Patent
Elektronische Ressource
Englisch
VIBROTACTILE SYSTEMS FOR AIRCRAFT, METHODS FOR OPERATING THE SAME, AND EJECTION SEATS
Europäisches Patentamt | 2023
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