中国民航大学学报 ›› 2013, Vol. 31 ›› Issue (3): 1-5.

• 民用航空 •    下一篇

基于航线对象的五边进近调配程序模型研究

赵嶷飞,刘然,王红勇   

  1. (中国民航大学国家空管运行安全技术重点实验室,天津300300)
  • 收稿日期:2012-05-04 修回日期:2012-08-10 出版日期:2013-06-23 发布日期:2013-10-08
  • 作者简介:赵嶷飞(1971—),男,湖南常德人,教授,博士,研究方向为空中交通规划与管理.
  • 基金资助:

    国家科技支撑计划(2011BAH24B10);国家自然科学基金项目(61039001);中国民用航空局科技基金项目(MHRD200913);中央高校基本
    科研业务费专项(ZXH2010C010,ZXH2009A004)

Analysis of final approach deployment procedures based on path objects

ZHAO Yi-fei,LIU Ran,WANG Hong-yong   

  1. (National Key Laboratory for Air Traffic Management Operation Safe Technology,CAUC,Tianjin 300300,China)
  • Received:2012-05-04 Revised:2012-08-10 Online:2013-06-23 Published:2013-10-08

摘要:

针对进近管制飞行密集、潜在冲突多、调配难度大的特点,提出一种智能化的调配程序研究方法。将五边调配程序分解为基本的飞行程序,并引入航线对象的概念,结合五边进近飞行特点建立调配程序的参数模型。通过模型计算得到关键位置点及飞行控制参数信息,同时生成飞行路径,综合全部信息即得到完整的调配方案,能够为实际管制工作提供参考和服务。计算机仿真结果证明了理论方法的可行性。

关键词: 空中交通管制, 五边进近, 调配, 航线对象, 飞行参数

Abstract:

For the fact that approach control is characterized by high flight-density, numerous potential conflicts and large deployment difficulty, an intelligent deployment procedure is proposed. To establish a parameter model, the final approach deployment procedure is divided into several basic flight procedures, combined with the concept of path objects and the features of final approach flight. By model calculating, we can collect information of the key location points as well as flight control parameters, and generate the flight path; all the data are integrated to form a complete deployment scheme, which can provide reference and service for the actual flight controlling practice. Feasibility of the theoretical method has been proved through simulation calculation.

Key words: air traffic control, final approach, deployment, path objects, flight parameter

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