Modeling and Parameter Identification of the Slung Load System of an Unmanned Rotorcraft using a Flexible Cable

In this paper, we propose a method to identify the parameters of a rotorcraft slung load system using the modal characteristics of a flexible cable. The proposed method estimates the length of the cable and the mass of the payload by means of a frequency analysis. Dynamic equations of the slung load...

Full description

Saved in:

Bibliographic Details
Published in:	International journal of aeronautical and space sciences Vol. 18; no. 2; pp. 365 - 377
Main Authors:	Lee, Byung-Yoon, Moon, Gun-Hee, Lee, Dong-Yeon, Tahk, Min-Jea, Oh, Hyun-Shik
Format:	Journal Article
Language:	English
Published:	한국항공우주학회 01.06.2017
Subjects:	항공우주공학 Slung Load System Udwadia-Kalaba Equation (UKE) Parameter Identification Flexible Cable
ISSN:	2093-274X, 2093-2480
Online Access:	Get full text
Tags:	Add Tag No Tags, Be the first to tag this record!

Be the first to leave a comment!