不确定随机规划模型

Q3 Engineering
Georgy Veresnikov, L. Pankova, V. Pronina
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引用次数: 1

摘要

本文提出了参数混合不确定性条件下的带约束优化模型——经验不确定性和认识不确定性。我们通过从统计数据中获得的具有概率分布函数的随机值来对具有概率不确定性的参数进行建模。我们通过刘的不确定性理论中引入的不确定性值来建模具有认知不确定性的参数。专家定义了不确定性分布函数。我们用不确定随机值对随机和不确定参数的函数进行建模,解释为由随机值参数化的认识值。优化标准(目标函数的确定性重复)是随机值和不确定值的不同特征的组合,既可以对目标函数求平均值,也可以考虑随机值和非确定值的可变性引起的风险或可靠性。使用所提出的不确定随机规划模型,我们将其形式化为带约束的双准则优化问题,并解决了参数混合不确定性条件下的初步空气动力学设计任务——飞机重量参数的计算。不确定性理论使得在某些条件下(对于足够宽的函数类)获得不确定函数特性的分析表达式成为可能,这显著降低了计算成本。为了计算飞机的重量参数,我们使用了多准则遗传算法和统计建模。我们研究了优化结果对随机值的给定概率水平的依赖性,以及反映所获得解的可靠性的认知值的专家置信度。作为应用所提出的模型计算飞机重量参数的结果,我们获得了图中所示的Pareto前沿。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Models Of Uncertain-Random Programming
The article proposes the models of optimization with constraints under conditions of parametric mixed uncertainty ‒ aleatory and epistemic. We model parameters with aleatory uncertainty by random values with probability distribution functions obtained from statistical data. We model parameters with epistemic uncertainty by uncertain values introduced in the uncertainty theory of Liu B. Experts define the uncertainty distribution functions. We model a function of random and uncertain parameters by uncertain-random value, interpreted as epistemic value parameterized by random values. Optimization criteria (deterministic duplicates of objective functions) are combination of different characteristics of random and uncertain values, which allows both to average objective functions and to take into account risks or reliability arising from the variability of random and uncertain values. Using the proposed models of uncertain-random programming, we formalized as a two-criterion optimization problem with constraints and solved the task of preliminary aerodynamic design in the conditions of parametric mixed uncertainty ‒ calculation of aircraft weight parameters. The uncertainty theory makes possible under certain conditions (for sufficiently wide class of functions) to obtain analytical expressions for characteristics of uncertain functions, that significantly reduces computational costs. To calculate weight parameters of aircraft, we use multicriteria genetic algorithm and statistical modeling. We investigate the dependence of the optimization result on the given probability levels for random values and the expert belief degree for epistemic values reflecting the reliability of the obtained solution. As result of applying the proposed models for calculating the weight parameters of the aircraft, we obtained the Pareto fronts shown in the figures.
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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
自引率
0.00%
发文量
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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