Systems and methods for issuing a hard landing warning and providing maintenance advisories for hard landing incidents

An aircraft (100) is provided. The aircraft may include, but is not limited to, an accelerometer (160) configured to measure a deceleration experienced by the aircraft (100) and a processor (120) coupled to the accelerometer (160). The processor (120) may be configured to determine if the aircraft (...

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Bibliographische Detailangaben

Hauptverfasser:	Lad, Girish M, Chandran, Nagarajan
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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