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Control of Future Air Traffic Systems via Complexity Bound Management

机译:通过复杂性边界管理控制未来的空中交通系统

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The complexity of the present system for managing air traffic has led to "discreteness" in approaches to creating new concepts: new concepts are created as point designs, based on experience, expertise, and creativity of the proposer. Discrete point designs may be highly successful but they are difficult to substantiate in the face of equally strong substantiation of competing concepts, as well as the state of the art in concept evaluation via simulations. Hybrid concepts may present a compromise - the golden middle. Yet a hybrid of sometimes in principle incompatible concepts forms another point design that faces the challenge of substantiation and validation. We are faced with the need to re-design the air transportation system ab initio. This is a daunting task, especially considering the problem of transitioning from the present system to any fundamentally new system. However, design from scratch is also an opportunity to reconsider approaches to new concept development. In this position paper we propose an approach, Optimized Parametric Functional Design, for systematic development of concepts for management and control of airspace systems, based on optimization formulations in terms of required system functions and states. This reasoning framework, realizable in the context of ab initio system design, offers an approach to deriving substantiated airspace management and control concepts. With growing computational power, we hope that the approach will also yield a methodology for actual dynamic control of airspace.
机译:用于管理空中交通的本系统的复杂性已经导致创建新概念的方法中的“离散性”:基于提议者的经验,专业知识和创造力,将新概念作为点设计来创建。离散点设计可能会非常成功,但面对竞争性概念的同样强有力的证明以及通过仿真进行概念评估的最新技术时,离散化的设计很难证明。混合概念可能会提出妥协-黄金中间。然而,有时原则上不兼容的概念的混合体构成了另一种点设计,该点设计面临着证实和验证的挑战。我们面临着从头开始重新设计航空运输系统的需求。这是一项艰巨的任务,尤其是考虑到从当前系统过渡到任何根本上新的系统的问题。但是,从头开始的设计也是重新考虑新概念开发方法的机会。在本立场文件中,我们提出了一种方法,即优化参数功能设计,用于根据所需系统功能和状态的优化公式,对空域系统的管理和控制概念进行系统开发。这种推理框架可在从头算系统设计的背景下实现,它提供了一种推导可靠的空域管理和控制概念的方法。随着计算能力的提高,我们希望该方法还将产生一种用于空域实际动态控制的方法。

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