Performance-based navigation (PBN) with continuous descent operations (CDO) for efficient approach over highly protected zones

A. Errico, V. Di Vito
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引用次数: 10

Abstract

This paper aims to demonstrate the benefits of combining the PBN concept with the CDA implementation by proposing an innovative system for the automatic generation of Curved and Continuous Descent Approach (CCDA) trajectories. These trajectories reduce aircraft fuel consumption and noise impact near to airport. Furthermore, the path curvature property preserves the dispersion of tracks with respect to the conventional ground-based step-down arrival path in both lateral and vertical profiles. The proposed system implements the procedure described in the following. First, specific paths are elaborated, with calculated top of descent point according to predefined angle or with initial fixed altitude up to intercept the descend glide path at constant or variable angle. This elaboration integrates obstacles geo-referenced mapping to avoid potential conflicts with airport/external environmental constraints by automatically generating corrective maneuvers. Then, the BADA aircraft performance parameters are elaborated in order to compute the fuel consumption associated to each calculated descent path. Finally, the CCDA path that minimizes the fuel consumption is selected. The system performances are evaluated in terms of fuel efficiency, noise impact, and lateral and vertical protected areas for tracking tolerance.
基于性能的导航(PBN)和连续下降操作(CDO)在高度保护区的有效进近
本文旨在通过提出一种自动生成曲线和连续下降方法(CCDA)轨迹的创新系统,证明将PBN概念与CDA实现相结合的好处。这些轨迹减少了飞机在机场附近的燃油消耗和噪音影响。此外,路径曲率特性在横向和垂直剖面上都保留了相对于传统地面降压到达路径的轨迹弥散。所提出的系统实现了如下所述的程序。首先,详细阐述具体路径,根据预定角度计算下降点顶部或初始固定高度向上拦截恒定或变角度的下降下滑路径。该系统集成了障碍物地理参考映射,通过自动生成纠正机动来避免与机场/外部环境约束的潜在冲突。然后,详细阐述了BADA飞机的性能参数,计算了每条下降路径的油耗。最后,选择燃油消耗最小的CCDA路径。根据燃油效率、噪音影响、横向和纵向跟踪公差的保护区域对系统性能进行评估。
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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