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首页> 外文期刊>Journal of Aerospace Sciences and Technologies >GUIDANCE OF FLIGHT PATH IN TMA DURING LANDING - A DESIGN STUDY
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GUIDANCE OF FLIGHT PATH IN TMA DURING LANDING - A DESIGN STUDY

机译：TMA着陆期间TMA飞行路径的指导-设计研究

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摘要

Air traffic has grown over the last few decades and is increasing further to a state where many airports and especially big hubs are reaching their limits of capacity. Hence many research activities were initiated to come up with more efficient and safe flight operations including Flight Path Boundary approach for controlling Time-of-Arrival in the terminal area. The design studies presented in this paper investigate a simplified representation of an intermediate flight path in the Vertical Situation Display for meeting the Time-of-Arrival requirements. A guidance law for maintaining constant EAS during descent has been evolved to adjust the thrust based on variation of air data measurements. Simulation results for typical case studies are presented to validate the approach. Possible areas for further extension are highlighted.
机译：在过去的几十年中，空中交通量有所增长，并且在许多机场，尤其是大型枢纽达到其容量极限的状态下，航空交通量进一步增加。因此，启动了许多研究活动以提供更高效，更安全的飞行操作，包括控制航站楼到达时间的飞行路线边界方法。本文提出的设计研究研究了垂直态势显示器中的中间飞行路径的简化表示，以满足到达时间的要求。已经制定了用于在下降期间保持恒定EAS的指导律，以根据空气数据测量值的变化来调整推力。给出了典型案例研究的仿真结果以验证该方法。突出显示了可能进一步扩展的区域。

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    M. Roshini; B. Subba Reddy;

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    VTU Extension Centre - Honeywell Honeywell Technology Solutions Lab Pvt Ltd No. 151/1, Doraisanipalya, Bannerghatta Road Bangalore-560 076, India;

    VTU Extension Centre - Honeywell Honeywell Technology Solutions Lab Pvt Ltd No. 151/1, Doraisanipalya, Bannerghatta Road Bangalore-560 076, India;

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