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An Optimal Strategy for Persistent Contrail Avoidance

机译:持续矛盾避免的最佳策略

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Persistent contrails have been recognized as a potential threat to the global climate. This paper presents a methodology to optimally reroute aircraft trajectories to avoid the formation of persistent contrails with the use of mixed integer programming (MIP). The main contributions of this paper are the introduction of a more realistic fuel burn model, and the implementation of a quadratic cost function. Existing MIP path planning literature has used a 1-norm approximation of the vehicle acceleration for fuel burn. The fuel burn model created for this paper is based on aircraft data and engine performance software, and the fuel burn cost was approximated with piecewise linear, and quadratic functions for implementation into the MIP. Fuel optimal trajectories for contrail avoidance were created for each cost function and the results were compared. In addition, differences between the linear and quadratic cost were investigated with a pathological obstacle field, and the sensitivity of the trajectory to changes in the planning horizon length and time step size are presented. For a specific scenario, it was found that persistent contrails could be avoided with a 2.76% increase in fuel burn.
机译:持续矛盾被认为是对全球气候的潜在威胁。本文介绍了最佳的飞机轨迹的方法,以避免使用混合整数编程(MIP)形成持久性凝结。本文的主要贡献是引入更现实的燃料燃烧模型,以及二次成本函数的实施。现有的MIP路径规划文献使用了一种用于燃料燃烧的车辆加速度的1范数近似。为此论文创建的燃料燃烧模型是基于飞机数据和发动机性能软件,燃料燃烧成本近似于分段线性,并将二次函数实现进入MIP。为每个成本函数创建抵果避免的燃料最佳轨迹,并比较结果。此外,通过病理障碍场研究了线性和二次成本之间的差异,并提出了轨迹对规划地平线长度和时间步长的变化的敏感性。对于特定方案,发现可以避免持续凝结尾迹,燃料燃烧增加2.76%。

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