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Next generation flight management system for real-time trajectory based operations

机译:用于基于实时轨迹的操作的下一代飞行管理系统

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摘要

This paper presents the concept of operations, architecture and trajectory optimisation algorithms of a Next Generation Flight Management System (NG-FMS). The NG-FMS is developed for Four Dimensional (4D) Intent Based Operations (IBO) in the next generation Communications, Navigation, Surveillance and Air Traffic Management system (CNS+A) context. The NG-FMS, primarily responsible for the aircraft navigation and guidance task, acts as a key enabler for achieving higher level of operational efficiency and mitigating environmental impacts both in manned and unmanned aircraft applications. The NG-FMS is interoperable with the future ground based 4DT Planning, Negotiation and Validation (4-PNV) systems, enabling automated Trajectory/Intent Based Operations (TBO/IBO). After the NG-FMS architecture is presented, the key mathematical models describing the trajectory generation and optimisation modes are introduced. A detailed error analysis is performed and the uncertainties affecting the nominal trajectories are studied to obtain the total NG-FMS error budgets. These are compared with the Required Navigation Performance (RNP) values for the various operational flight tasks considered.
机译:本文介绍了下一代飞行管理系统(NG-FMS)的操作,架构和轨迹优化算法的概念。 NG-FMS是在下一代通信,导航,监视和空中交通管理系统(CNS + A)上下文中为基于四维(4D)基于意图的操作(IBO)开发的。 NG-FMS主要负责飞机的导航和制导任务,是在无人驾驶和无人驾驶飞机应用中实现更高水平的运营效率并减轻环境影响的关键推动力。 NG-FMS可与未来的地面4DT规划,协商和确认(4-PNV)系统互操作,从而实现基于轨迹/意图的自动操作(TBO / IBO)。提出了NG-FMS体系结构后,介绍了描述轨迹生成和优化模式的关键数学模型。进行了详细的误差分析,并研究了影响标称轨迹的不确定性,以获得总的NG-FMS误差预算。将这些与考虑的各种操作飞行任务的“所需导航性能”(RNP)值进行比较。

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