A modified hybrid uncertain analysis method for dynamic response field of the LSOAAC with random and interval parameters

被引:26
|
作者
Zi, Bin [1 ]
Zhou, Bin [1 ]
机构
[1] Hefei Univ Technol, Sch Mech & Automot Engn, 193 Tunxi Rd, Hefei 230009, Peoples R China
基金
中国国家自然科学基金;
关键词
Dynamic response field; Luffing system of an automobile crane; Modified hybrid uncertain analysis method; Hybrid Monte Carlo method; Random interval moment method; FINITE-ELEMENT; PREDICTION; FUZZY; CRANE; SYSTEMS;
D O I
10.1016/j.jsv.2016.03.032
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
For the prediction of dynamic response field of the luffing system of an automobile crane (LSOAAC) with random and interval parameters, a hybrid uncertain model is introduced. In the hybrid uncertain model, the parameters with certain probability distribution are modeled as random variables, whereas, the parameters with lower and upper bounds are modeled as interval variables instead of given precise values. Based on the hybrid uncertain model, the hybrid uncertain dynamic response equilibrium equation, in which different random and interval parameters are simultaneously included in input and output terms, is constructed. Then a modified hybrid uncertain analysis method (MHUAM) is proposed. In the MHUAM, based on random interval perturbation method, the first-order Taylor series expansion and the first-order Neumann series, the dynamic response expression of the LSOAAC is developed. Moreover, the mathematical characteristics of extrema of bounds of dynamic response are determined by random interval moment method and monotonic analysis technique. Compared with the hybrid Monte Carlo method (HMCM) and interval perturbation method (IPM), numerical results show the feasibility and efficiency of the MHUAM for solving the hybrid LSOAAC problems. The effects of different uncertain models and parameters on the LSOAAC response field are also investigated deeply, and numerical results indicate that the impact made by the randomness in the thrust of the luffing cylinder F is larger than that made by the gravity of the weight in suspension Q. In addition, the impact made by the uncertainty in the displacement between the lower end of the lifting arm and the luffing cylinder a is larger than that made by the length of the lifting arm L. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:111 / 137
页数:27
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