Trajectory computation Infrastructure based on BADA Aircraft Performance Model

E. Gallo, J. Lopez-Leones, M. Vilaplana, F.A. Navarro, A. Nuić
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引用次数: 33

Abstract

A more predictable Air Traffic Management (ATM) system based on automation requires a precise Trajectory Computation Infrastructure (TCI). The accuracy of the computed trajectories does not only depend on the TCI trajectory integration capabilities, but also on the input received from the associated Aircraft Performance Model (APM), the operational instructions defining each trajectory, and the atmospheric data. EUROCONTROL Experimental Centre (EEC) conducts a number of activities in the domain of APMs, which are performed within the scope of Base of Aircraft Data (BADA). EEC has been supported by Boeing Research & Technology Europe (BR&TE) in the definition, development, implementation, and evaluation of an advanced APM suitable for the stringent requirements of future trajectory prediction tools. This new APM will become version 4.0 of BADA, released and maintained by EEC. BR&TE has also supported EEC in the design and development of an advanced bidimensional (vertical plane) TCI intended to exploit all the BADA 4.0 APM capabilities. This TCI accepts either a BADA 4.0 or a BADA 3.x APM, together with all kinds of winds, as well as temperature and pressure deviations over the International Standard Atmosphere (ISA). The TCI requires five simultaneous operational instructions to compute any trajectory segment. These instructions model the commands issued by the flight deck, and comprise the "aircraft intent" (AI). Three of them set the position of the landing gear, high lift devices, and speed brakes, while the other two determine the aircraft motion in the vertical plane. Accepted instructions include different speed, energy, altitude, vertical speed, path angle, and throttle laws, and even optimum speed laws intended to maximize certain flight characteristics, such as range or cost. This paper presents the TCI capabilities and interfaces. It describes the different elements involved in the trajectory computation process, placing special emphasis in the instructions comprising the AI and how they can be combined, as well as the equations describing the aircraft motion and their integration. It also includes an example of the trajectory computation process.
基于BADA飞机性能模型的弹道计算基础架构
基于自动化的空中交通管理(ATM)系统需要精确的轨迹计算基础设施(TCI)。计算轨迹的准确性不仅取决于TCI轨迹集成能力,还取决于从相关飞机性能模型(APM)接收的输入、定义每个轨迹的操作指令以及大气数据。欧洲控制实验中心(EEC)在飞机数据基地(BADA)的范围内开展了许多apm领域的活动。EEC已经得到波音欧洲研究与技术公司(BR&TE)的支持,用于定义、开发、实施和评估一种先进的APM,该APM适用于未来轨道预测工具的严格要求。这个新的APM将成为BADA的4.0版本,由EEC发布和维护。BR&TE还支持EEC设计和开发先进的二维(垂直平面)TCI,旨在利用BADA 4.0 APM的所有功能。这个TCI接受BADA 4.0或BADA 3。x APM,以及各种风,以及国际标准大气(ISA)上的温度和压力偏差。TCI需要五个同时操作指令来计算任何轨迹段。这些指令模拟了飞行甲板发出的命令,并组成了“飞机意图”(AI)。其中三个设置起落架,高升力装置和速度制动器的位置,而另外两个确定飞机在垂直平面上的运动。可接受的指令包括不同的速度、能量、高度、垂直速度、路径角度和油门定律,甚至是旨在最大化某些飞行特性(如航程或成本)的最佳速度定律。本文介绍了TCI的功能和接口。它描述了轨迹计算过程中涉及的不同元素,特别强调了包含AI的指令以及它们如何组合,以及描述飞机运动及其集成的方程。文中还给出了弹道计算过程的实例。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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