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Comparison of aircraft models and integration schemes for interval management in the tracon

机译:tracon中用于间隔管理的飞机模型和集成方案的比较

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Reusable models of common elements for communication, computation, decision and control in air traffic management are necessary in order to enable simulation, analysis and assurance of emergent properties, such as safety and stability, for a given operational concept. Uncertainties due to faults, such as dropped messages, along with non-linearities and sensor noise are an integral part of these models, and impact emergent system behavior. Flight control algorithms designed using a linearized version of the flight mechanics will exhibit error due to model uncertainty, and may not be stable outside a neighborhood of the given point of linearization. Moreover, the communication mechanism by which the sensed state of an aircraft is fed back to a flight control system (such as an ADS-B message) impacts the overall system behavior; both due to sensor noise as well as dropped messages (vacant samples). Additionally simulation of the flight controller system can exhibit further numerical instability, due to selection of the integration scheme and approximations made in the flight dynamics. We examine the theoretical and numerical stability of a speed controller under the Euler and Runge-Kutta schemes of integration, for the ‘Maintain’ phase for a “Mid-Term (2035–2045) Interval Management (IM) Operational Concept” for descent and landing operations. We model uncertainties in communication due to missed ADS-B messages by vacant samples in the integration schemes, and compare the emergent behavior of the system, in terms of stability, via the boundedness of the final system state. Any bound on the errors incurred by these uncertainties will play an essential part in a composable assurance argument required for real-time, flight-deck guidance and control systems,. Thus, we believe that the creation of reusable models, which possess property guarantees, such as safety and stability, is an innovative and essential requirement to assessing - he emergent properties of novel airspace concepts of operation.
机译:空中交通管理中用于通信,计算,决策和控制的通用元素的可重用模型是必要的,以便能够对给定的操作概念进行仿真,分析和保证紧急特性(例如安全性和稳定性)。由于故障而导致的不确定性,例如消息丢失,非线性和传感器噪声,都是这些模型不可或缺的一部分,并且会影响紧急系统的行为。使用线性化的飞行力学版本设计的飞行控制算法会因模型不确定性而表现出误差,并且在给定的线性化点附近无法保持稳定。此外,将飞机的感知状态反馈到飞行控制系统的通信机制(例如ADS-B消息)会影响整个系统的行为。都是由于传感器噪声以及消息丢失(空样本)造成的。另外,由于选择了集成方案和飞行动力学中的近似值,飞行控制器系统的仿真可能会显示出进一步的数值不稳定性。我们研究了在Euler和Runge-Kutta集成方案下速度控制器的理论和数值稳定性,用于“维持”阶段的“中期(2035–2045)间隔管理(IM)操作概念”的下降和下降。着陆行动。我们对由于集成方案中的空缺样本而丢失了ADS-B消息而造成的通信不确定性进行建模,并通过最终系统状态的有界性来比较系统在稳定性方面的紧急行为。由这些不确定性引起的误差的任何界限将在实时,驾驶舱制导和控制系统所需的可组合保证论据中发挥重要作用。因此,我们认为创建具有属性保证(例如安全性和稳定性)的可重用模型是评估的创新性和必要条件-他对新型空域作战概念的新兴属性进行了评估。

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