全球观测系统(IAGOS)项目中在役飞机实际飞行轨迹和时间优化飞行轨迹的比较

IF 0.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE
O. Boucher, N. Bellouin, H. Clark, E. Gryspeerdt, Julien Karadayi
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引用次数: 0

摘要

航空公司优化飞行轨迹是为了最大限度地降低运营成本,其中燃料消耗是一个很大的贡献者。众所周知,由于空域拥挤和限制、安全法规、恶劣天气和其他操作限制,飞行轨迹并非燃油最优。然而,轨迹在多大程度上不是燃料最优的(因此也不是二氧化碳最优的)还不为人所知。在本研究中,我们提出了两种优化飞行巡航时间的方法,即在给定的飞行高度和恒定的空速下充分利用风型。我们根据全球观测系统(IAGOS)项目在役飞机记录的实际飞行轨迹对这些方法进行了测试。一种方法比另一种方法更鲁棒(计算速度更快),但当成功时,两种方法非常吻合,最优值通常在0.1%左右。IAGOS的实际巡航轨迹平均比跨大西洋航线计算出的最优值长1%,考虑到实际轨迹的构造不可能比我们的最优值更好,这使得改进的空间很小。其他路线的平均非最优度较大,可达10%。在一些航线上,也存在未得到很好优化的离群航班;然而,其原因尚不清楚。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Comparison of Actual and Time-Optimized Flight Trajectories in the Context of the In-Service Aircraft for a Global Observing System (IAGOS) Programme
Airlines optimize flight trajectories in order to minimize their operational costs, of which fuel consumption is a large contributor. It is known that flight trajectories are not fuel-optimal because of airspace congestion and restrictions, safety regulations, bad weather and other operational constraints. However, the extent to which trajectories are not fuel-optimal (and therefore CO2-optimal) is not well known. In this study, we present two methods for optimizing the flight cruising time by taking best advantage of the wind pattern at a given flight level and for constant airspeed. We test these methods against actual flight trajectories recorded under the In-service Aircraft for a Global Observing System (IAGOS) programme. One method is more robust than the other (computationally faster) method, but when successful, the two methods agree very well with each other, with optima generally within the order of 0.1%. The IAGOS actual cruising trajectories are on average 1% longer than the computed optimal for the transatlantic route, which leaves little room for improvement given that by construction the actual trajectory cannot be better than our optimum. The average degree of non-optimality is larger for some other routes and can be up to 10%. On some routes, there are also outlier flights that are not well optimized; however, the reason for this is not known.
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来源期刊
Aerospace America
Aerospace America 工程技术-工程:宇航
自引率
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发文量
9
审稿时长
4-8 weeks
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