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Trajectory optimization algorithm for a constant altitude cruise flight with a required time of arrival constraints

机译:具有所需到达时间约束的恒定高度巡航飞行的轨迹优化算法

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Decreasing the flight costs, therefore flying along the optimal for a trajectory, is a constant preoccupation for all aircraft operators. Moreover, the reduction of fuel consumption and pollutant emissions is a significant factor in the trajectory optimization analysis. The study presented in this article is part of the research conducted at the Laboratoire de recherche en commande active, avionique et aeroservoelasticite (LARCASE), at Ecole de Technologie Superieure, in the field of aircraft trajectory optimization algorithms for Flight Management System platforms, and investigates an optimization algorithm for a leveled cruise flight segment with required time of arrival constraint. The proposed algorithm is deterministic, in accordance with the requirements for avionics equipment.
机译:降低飞行成本,从而沿着最优的轨迹飞行,一直是所有飞机运营商的首要任务。此外,减少燃料消耗和污染物排放是轨迹优化分析中的重要因素。本文介绍的研究是在高等技术学院的航空动力与航空弹性体实验室(LACASE)进行的研究的一部分,该研究涉及用于飞行管理系统平台的飞机轨迹优化算法,并进行了调查。具有所需到达时间约束的水平巡航航段的优化算法。根据航空电子设备的要求,所提出的算法是确定性的。

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