具有参数认识不确定性的初步设计

G. Veresnikov, L. Pankova, V. Pronina
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引用次数: 0

摘要

在设计中,特别是在初步设计中,参数准确性的假设是不合理的,因为这里的参数是不准确的(不确定的),这是由于知识不足或缺乏统计数据,以及设计参数在生产中以一定的公差进一步实施的事实。在参数不确定的条件下应用确定性优化方法可能导致不可接受的解决方案,即使参数略有变化。目前,为了说明参数的不确定性,有常用的随机方法设计用于说明随机参数的先验已知分布函数的偶然不确定性。然而,在初步设计中,大多数参数都不是具有已知分布函数的随机变量。有关参数的必要信息是从专家那里获得的。在本文中,我们开发了在缺乏知识和观察结果引起的认知不确定性条件下进行初步设计的方法和算法,并通过专家评估进行补充。本文考虑了在输入参数和设计参数具有认识不确定性的情况下的优化设计问题。刘的不确定性理论在解决初步设计问题上的选择是合理的。提出了设计参数不确定的模型和设计参数和输入参数不确定时的优化模型。利用该模型求解了超音速机动飞机推进系统参数的优化设计问题。将结果与蒙特卡罗方法的解进行了比较。使用所提出的模型的求解时间减少了两个数量级。
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Preliminary Design With the Epistemic Uncertainty of Parameters
In design, especially in preliminary design, the assumption of parameter accuracy is not justified, since the parameters here are inaccurate (uncertain), due to insufficient knowledge or lack of statistics, as well as the fact that design parameters are further implemented in the production with some tolerance. The application of deterministic optimization methods under conditions of parametric uncertainty can lead to unacceptable solutions even with slight variation in the parameters. Currently, to account for uncertainty of the parameters there are commonly used stochastic methods designed to account for aleatory uncertainty with a priori known distribution functions of random parameters. However, in the preliminary design, most of the parameters are not random variables with known distribution functions. The necessary information on the parameters is obtained from the experts. In this paper, we develop methods and algorithms for preliminary design in conditions of epistemic uncertainty arising from lack of knowledge and observation results, replenished by expert assessments. In the paper the problem of optimal design in the presence of input and design parameters with epistemic uncertainty is considered. The choice of Liu's uncertainty theory for solving the problems of preliminary design is justified. The model of uncertain design parameter and optimization model with uncertain design and input parameters are proposed. The task of optimal design of the propulsion system parameters of  supersonic maneuverable airplane is solved using the proposed models. The results are compared with the solution using Monte Carlo method. The solution time using the proposed model is two orders of magnitude less.
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来源期刊
Advances in Systems Science and Applications
Advances in Systems Science and Applications Engineering-Engineering (all)
CiteScore
1.20
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0.00%
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0
期刊介绍: Advances in Systems Science and Applications (ASSA) is an international peer-reviewed open-source online academic journal. Its scope covers all major aspects of systems (and processes) analysis, modeling, simulation, and control, ranging from theoretical and methodological developments to a large variety of application areas. Survey articles and innovative results are also welcome. ASSA is aimed at the audience of scientists, engineers and researchers working in the framework of these problems. ASSA should be a platform on which researchers will be able to communicate and discuss both their specialized issues and interdisciplinary problems of systems analysis and its applications in science and industry, including data science, artificial intelligence, material science, manufacturing, transportation, power and energy, ecology, corporate management, public governance, finance, and many others.
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