主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
FMS巡航阶段的垂直轨迹预测算法及应用
作者:
作者单位:

中国航空无线电电子研究所

作者简介:

通讯作者:

中图分类号:

V249

基金项目:


The vertical trajectory prediction algorithm of FMS for the cruise flight phase and its application
Author:
Affiliation:

Chinese Aeronautical Radio Electronics Research Institute

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    飞机的飞行过程涉及多个垂直飞行阶段,巡航阶段占了绝大部分的飞行时间、飞行距离及燃油消耗,研究飞行管理系统(FMS)巡航阶段的垂直轨迹预测算法,对于提升飞行的经济性、舒适性、安全性是非常重要和必要的。为了满足不同类型飞机之间巡航阶段垂直轨迹预测算法的通用性,提高垂直轨迹预测的精确度和可信度,提出一种适用于巡航阶段的垂直轨迹预测算法。首先,通过计算巡航阶段的速度剖面,构建预测过程中更加符合实际的大气模型;然后基于第一性原理(第一法则)的飞机模型计算所需的巡航燃油流量数据,通过设计的巡航阶段垂直轨迹预测算法逻辑,给出巡航阶段预测的垂直轨迹;最后通过地面仿真试验和空中试飞验证算法的有效性与准确性。结果表明:本文提出的基于第一性原理飞机模型的FMS 巡航阶段垂直轨迹预测算法能够预测飞机的巡航轨迹,且预测精度误差低于1%。

    Abstract:

    It is well known that there are several vertical flight phases for the aircraft in the flight. The cruise flight phase takes most of the flight time, flight distance and fuel consumption, so it is important and necessary to develop the FMS vertical trajectory prediction algorithm for the cruise flight phase, aiming to improve the economy, comfort and safety of the flight. In order to meet the versatility of the vertical trajectory prediction algorithm between different types of aircraft in the cruise phase and improve the accuracy and reliability of the prediction, the algorithm of vertical trajectory prediction for cruise flight phase is proposed in this paper. By calculating the cruise speed profile and constructing the realistic atmospheric model of prediction, and then calculating the cruise fuel flow data based on the aircraft model of first-principles, the vertical trajectory prediction for the cruise phase is given by designing the vertical trajectory prediction algorithm logic. Finally, the effectiveness and accuracy of the algorithm are verified by ground simulation and air flight test. The results show that the vertical trajectory prediction algorithm of FMS cruise phase based on the aircraft model of first-principles can predict the cruise trajectory of the aircraft, and the prediction accuracy error is less than 1%.

    参考文献
    相似文献
    引证文献
引用本文

郑起彪,迟哲敏,陈祺,齐林. FMS巡航阶段的垂直轨迹预测算法及应用[J].航空工程进展,2024,15(2):166-172

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2023-06-20
  • 最后修改日期:2023-11-20
  • 录用日期:2023-12-12
  • 在线发布日期: 2024-03-08
  • 出版日期: