Design and validation of the evolved version of the tactical separation system

IF 1.2 4区 工程技术 Q3 ENGINEERING, AEROSPACE Aircraft Engineering and Aerospace Technology Pub Date : 2024-05-27 DOI:10.1108/aeat-03-2024-0080
V. Di Vito, G. Torrano, G. Cerasuolo, M. Ferrucci
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Abstract

Purpose The small air transport (SAT) domain is gaining increasing interest over the past decade, based on its perspective relevance in enabling efficient travel over a regional range, by exploiting small airports and fixed wing aircraft with up to 19 seats (EASA CS-23 category). To support its wider adoption, it is needed to enable single pilot operations. Design/methodology/approach An integrated mission management system (IMMS) has been designed and implemented, able to automatically optimize the aircraft path by considering trajectory optimization needs. It takes into account both traffic scenario and weather actual and forecasted condition and is also able to select best destination airport, should pilot incapacitation occur during flight. As part of the IMMS, dedicated evolved tactical separation system (Evo-TSS) has been designed to provide elaboration of both surrounding and far located traffic and subsequent traffic clustering, to support the trajectory planning/re-planning by the IMMS. Findings The Clean Sky 2-funded project COAST (Cost Optimized Avionics SysTem) successfully designed and validated through flight demonstrations relevant technologies enabling affordable cockpit and avionics and supporting single pilot operations for SAT vehicles. These technologies include the TSS in its baseline and evolved versions, included in the IMMS. Originality/value This paper describes the TSS baseline version and the basic aspects of the Evo-TSS design. It is aimed to outline the implementation of the Evo-TSS dedicated software in Matlab/Simulink environment, the planned laboratory validation campaign and the results of the validation exercises in fast-time Matlab/Simulink environment, which were successfully concluded in 2023.
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设计和验证改进版战术分离系统
目的小型航空运输(SAT)领域在过去十年中日益受到关注,这是因为它可以利用小型机场和最多 19 个座位的固定翼飞机(EASA CS-23 类别),在区域范围内实现高效旅行。为了支持其更广泛的应用,需要实现单人驾驶。设计/方法/途径设计并实施了一个综合任务管理系统(IMMS),能够通过考虑轨迹优化需求自动优化飞机路径。该系统同时考虑了交通情况和天气的实际和预测状况,还能在飞行过程中飞行员丧失能力的情况下选择最佳目的地机场。作为 IMMS 的一部分,设计了专用的进化战术分离系统 (Evo-TSS),以提供周围和远处交通的详细情况以及随后的交通集群,从而为 IMMS 的轨迹规划/重新规划提供支持。研究结果洁净天空 2 号资助项目 COAST(成本优化航空电子系统)成功设计并通过飞行演示验证了相关技术,从而为 SAT 飞行器提供了经济实惠的驾驶舱和航空电子设备,并支持单人驾驶操作。这些技术包括 TSS 的基线版和进化版,已纳入 IMMS。本文旨在概述 Evo-TSS 专用软件在 Matlab/Simulink 环境中的实施情况、计划进行的实验室验证活动以及在快速 Matlab/Simulink 环境中进行的验证活动的结果,这些活动已于 2023 年圆满结束。
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来源期刊
Aircraft Engineering and Aerospace Technology
Aircraft Engineering and Aerospace Technology 工程技术-工程:宇航
CiteScore
3.20
自引率
13.30%
发文量
168
审稿时长
8 months
期刊介绍: Aircraft Engineering and Aerospace Technology provides a broad coverage of the materials and techniques employed in the aircraft and aerospace industry. Its international perspectives allow readers to keep up to date with current thinking and developments in critical areas such as coping with increasingly overcrowded airways, the development of new materials, recent breakthroughs in navigation technology - and more.
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