中国民航大学学报 ›› 2026, Vol. 44 ›› Issue (3): 30-38.

• 民机安全性与适航 • 上一篇    下一篇

混合构型跑道复飞与离场航空器碰撞风险研究

  

  1. (1. 中国民航大学空中交通管理学院,天津 300300;2.中国民用航空华北地区空中交通管理局终端管制室,北京 100621)
  • 收稿日期:2025-03-27 修回日期:2025-05-30 出版日期:2026-06-30 发布日期:2026-07-03
  • 作者简介:杨群亭(1983— ),男,河南南阳人,讲师,博士,研究方向为交通运输. 
  • 基金资助:
    西藏自治区重大科技专项(XZ202402ZD0004);天津市科技计划项目(23JCYBJC00050);中央高校基本科研业务费专项(3122017064)

Study on collision risk between go-around and departing aircraft on mixed configuration runways

  1. (1. College of Air Traffic Management, CAUC, Tianjin 300300, China; 2. Approach Control Unit, Air Traffic Management Bureau of North
  • Received:2025-03-27 Revised:2025-05-30 Online:2026-06-30 Published:2026-07-03

摘要: 为解决复飞航空器在定高转弯程序下转弯位置不确定的问题,首先,本文基于不同高度复飞情况,建立了航 空器运动学模型;其次,结合侧向跑道离场航空器的位置变化,构建实时动态间隔计算模型,并进一步引入 位置误差,建立碰撞风险模型;最后,以成都天府国际机场为例,分析了进近航空器复飞时与侧向跑道离场 航空器的碰撞风险。研究结果表明,在RWY20的运行条件下,碰撞风险与进近航空器复飞位置显著相关, 合理设定起降窗口(ADW,arrival-departure window)(跑道入口前 7 900 m 至入口后 900 m)可有效提升运行 安全。此外,复飞性能参数对ADW范围有重要影响,随着爬升梯度增大,ADW的范围可相应减小。

关键词: 碰撞风险, 位置误差, 复飞, 混合构型跑道, 起降窗口(ADW)

Abstract:  To address the issue of uncertain turning positions for go-around aircraft during fixed-altitude turning proce鄄 dures, a kinematic model of the aircraft was first established based on different altitude go-around situations in this paper. Secondly, combining the position changes of aircraft departing from the lateral runway, a real-time dynamic interval calculation model was constructed, and position errors were further introduced to establish a collision risk model. Finally, taking Chengdu Tianfu International Airport as a case study, the collision risk be鄄 tween approach aircraft during go-around and aircraft departing from the lateral runway was analyzed. The re鄄 search results indicate that under the operating conditions of RWY 20, the collision risk is significantly correlated with the approach aircraft′s go-around position. Reasonably setting the arrival-departure window (ADW), from 7 900 m before the runway threshold to 900 m beyond it, can effectively improve operational safety. In addition, the go-around performance parameters have a significant impact on the ADW range, and as the climb gradient increases, the ADW range can correspondingly decrease.

Key words: collision risk, position error, go-around, mixed configuration runway, arrival-departure window (ADW)

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