contributor author | Joseph J. Hollkamp | |
contributor author | Stephen M. Batill | |
date accessioned | 2017-05-08T21:15:37Z | |
date available | 2017-05-08T21:15:37Z | |
date copyright | October 1990 | |
date issued | 1990 | |
identifier other | %28asce%290893-1321%281990%293%3A4%28271%29.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/44690 | |
description abstract | Discrete time‐series models can be used for the dynamic response prediction of linear structures. When structural nonlinearities are present, it may be possible to modify the form of the discrete time‐series model to account for the nonlinearities. One approach is to allow the model parameters to become functions of state. This paper explores some possible forms of the parameter functions for various nonlinear structures. Numerical case studies using both a Duffing oscillator and a combined viscous and coulomb damped oscillator are presented. Also, experimental data from a highly nonlinear aircraft landing gear strut are used to evaluate different model forms. The results from these studies show the potential for future applications of nonlinear time‐series models. | |
publisher | American Society of Civil Engineers | |
title | Time‐Series Models for Nonlinear Systems | |
type | Journal Paper | |
journal volume | 3 | |
journal issue | 4 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/(ASCE)0893-1321(1990)3:4(271) | |
tree | Journal of Aerospace Engineering:;1990:;Volume ( 003 ):;issue: 004 | |
contenttype | Fulltext | |