论文标题
一个基于模糊的框架,用于支持机甲系统的多准则设计
A Fuzzy-based Framework to Support Multicriteria Design of Mechatronic Systems
论文作者
论文摘要
设计机甲系统是一项复杂的任务,因为它在存在相互作用的设计目标的情况下处理了具有多学科性质的大量系统组件。当前,连续设计被设计师广泛使用,这些行业与不同的域及其相应的设计目标分别导致功能性,但不一定是最佳结果。因此,出现了系统和多目标设计方法的需求。作者先前已经提出了一种基于新概念设计的新概念设计方法,该方法先前介绍了该方法,该方法使用一系列非线性模糊的聚合功能来促进在存在相互作用标准的情况下进行设计评估的决策。 Choquet模糊积分是用于多准则决策的决策理论中使用的最富有表现力和最可靠的偏好模型之一。他们通过模糊措施对任何标准联盟分配权重的手段进行加权聚合。这使设计人员能够建模重要性以及标准之间的相互作用,从而涵盖了可能的决策结果。但是,模糊措施的规范涉及许多参数,并且仅依靠设计师的直觉非常困难。在本文中,我们讨论了针对机电设计过程量身定制的三种不同模糊度量识别方法,并通过设计视觉引导的四极管无人机的案例研究来说明。从每种方法获得的结果将在最后讨论。
Designing a mechatronic system is a complex task since it deals with a high number of system components with multi-disciplinary nature in the presence of interacting design objectives. Currently, the sequential design is widely used by designers in industries that deal with different domains and their corresponding design objectives separately leading to a functional but not necessarily an optimal result. Consequently, the need for a systematic and multi-objective design methodology arises. A new conceptual design approach based on a multi-criteria profile for mechatronic systems has been previously presented by the authors which uses a series of nonlinear fuzzy-based aggregation functions to facilitate decision-making for design evaluation in the presence of interacting criteria. Choquet fuzzy integrals are one of the most expressive and reliable preference models used in decision theory for multicriteria decision making. They perform a weighted aggregation by the means of fuzzy measures assigning a weight to any coalition of criteria. This enables the designers to model importance and also interactions among criteria thus covering an important range of possible decision outcomes. However, specification of the fuzzy measures involves many parameters and is very difficult when only relying on the designer's intuition. In this paper, we discuss three different methods of fuzzy measure identification tailored for a mechatronic design process and exemplified by a case study of designing a vision-guided quadrotor drone. The results obtained from each method are discussed in the end.