A system and method for identifying a slung load for an aircraft with one or more sensors includes receiving, with a processor via one or more sensors, sensor information related to flight dynamics data for the aircraft; determining, with the processor, control input commands for the aircraft in response to the receiving of the flight dynamics data; determining, with the processor, signals indicative of an estimated pendulum frequency; and determining, with the processor, parameters associated with the slung load in response to the determining of the estimated pendulum frequencies.
SLUNG LOAD IDENTIFICATION WITH AIRCRAFT FLIGHT DYNAMICS DATA
16.08.2018
Patent
Elektronische Ressource
Englisch
Slung load identification with aircraft flight dynamics data
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