中国民航大学学报 ›› 2019, Vol. 37 ›› Issue (3): 11-16.

• 民用航空 • 上一篇    下一篇

基于质量估算策略的离场飞机高度剖面预测#br#

康南1,韩孝兰2,胡杨2,魏志强2
  

  1. (1.中国民用航空局空管局空管部,北京100086; 2.中国民航大学空中交通管理学院,天津300300)

  • 出版日期:2019-06-27 发布日期:2020-04-01
  • 作者简介:康南(1971—),男,北京人,高级工程师,硕士,研究方向为空中交通管理.
  • 基金资助:
    国家自然科学基金项目(U1533116,U1633125);中央高校基本科研业务费专项(3122017067)

Departure aircraft altitude profile prediction based on aircraft mass estimation strategy#br#

KANG Nan1, HAN Xiaolan2, HU Yang2, WEI Zhiqiang2#br#   

  1. (1. Department of Air traffic, Air Traffic Management Bureau, CAAC, Beijing 100086, China;2. College of Air Traffic Management, CAUC, Tianjin 300300, China)
  • Online:2019-06-27 Published:2020-04-01

摘要: 离场飞机高度剖面预测无法直接获取飞机质量参数而影响预测精度。针对该问题,建立了基于实时航迹数据的飞机质量估算模型和高度剖面预测模型,利用二次雷达记录的B737-800 飞机真实离场航迹,从飞机离地高度500 m 开始,根据每一时刻的历史航迹数据实时估算飞机质量,之后不断预测后续离场的垂直航迹,并将预测航迹与真实航迹进行对比,分析离场时间和飞行距离的预测精度。结果表明,在进行质量估算时,所依据航迹数据的飞行高度越高,后续航迹预测精度也越高。在3 500 m 及以上高度开始质量估算,可使后续误差基本维持在5%以内(时间偏差不超过1 min,距离偏差不超过5 000 m)。

关键词: 航空运输, 航迹预测, 质量估算, 离场航迹

Abstract: The aircraft weight cannot be obtained directly from departure aircraft altitude profile prediction, and thus the precision accuracy is affected. Aiming at this problem, the aircraft weight estimation model and the altitude profile prediction model based on the real-time track data are established. Using the actual departure trajectory of B737-800 recorded by SSR, the aircrafts’ weight and profile is predicted in real time from 500 m above the ground according to the historical track data at each time. Then the vertical track of follow -up departure is predicted and compared with the actual trajectory to analyze the prediction accuracy of departure time and flight distance. Results show that higher prediction accuracy of aircraft weight can be achieved with trajectory parameters on higher flight altitudes. If the weight estimation is started on and above 3 500 m, the subsequent error can be maintained within 5%

Key words: air transportation, trajectory prediction, mass estimation, departure trajectory

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