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.


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    Title :

    Slung load identification with aircraft flight dynamics data


    Contributors:

    Publication date :

    2019-04-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL



    SLUNG LOAD IDENTIFICATION WITH AIRCRAFT FLIGHT DYNAMICS DATA

    SANE HARSHAD S / CONNOR MICHAEL AARON / CHEREPINSKY IGOR | European Patent Office | 2018

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    Flight Dynamic Characteristics of Tiltrotor Aircraft Slung-Load System

    Cao, Yihua / Qi, Qi / Zhang, Dongfang | AIAA | 2017



    Dynamics of a slung load

    FEASTER, L. / U.S. Army / Washington et al. | AIAA | 1977