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Fuel burn prediction algorithm for cruise, constant speed and level flight segments

机译:巡航,恒定速度和水平飞行段的燃油消耗预测算法

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摘要

This paper presents a new algorithm that predicts the quantity of fuel burned by an aircraft flying at a constant speed and altitude. It considers the continuous fuel burn rate variation with time caused by the gross weight (and centre of gravity position) modification due to the fuel burn process itself. The algorithm was developed for use by the Flight Management System (FMS) and employs the same aircraft performance data as the existing FMS fuel burn prediction algorithms. The new fuel burn method was developed for aircraft models that use the centre of gravity position as well as for models that do not consider the centre of gravity position. This algorithm was developed for normal flight conditions. Algorithm performances were evaluated for two aircraft models: one for models that use an aircraft's centre of gravity position - a more complex and computing intensive method, and one for those that do not use the centre of gravity position. The validation data were generated based on the information produced on a CMC Electronics - Esterline FMS platform that used identical aircraft models and performance data for identical flight conditions.
机译:本文提出了一种新算法,该算法可预测以恒定速度和高度飞行的飞机燃烧的燃油量。它考虑了由于燃油燃烧过程本身引起的毛重(和重心位置)变化而导致的连续燃油燃烧率随时间的变化。该算法是为供飞行管理系统(FMS)使用而开发的,并采用了与现有FMS燃油消耗预测算法相同的飞机性能数据。新的燃油燃烧方法是针对使用重心位置的飞机模型以及不考虑重心位置的模型开发的。该算法是针对正常飞行条件开发的。对两种飞机模型的算法性能进行了评估:一种模型用于使用飞机重心位置的模型-一种更复杂且计算量大的方法,另一种模型用于不使用重心位置的模型。验证数据是基于在CMC Electronics-Esterline FMS平台上生成的信息生成的,该平台使用相同的飞机模型和相同的飞行条件下的性能数据。

著录项

  • 来源
    《The Aeronautical Journal》 |2013年第1191期|491-504|共14页
  • 作者单位

    Ecole de Technologie Superieure Montreal, Quebec Canada;

    Ecole de Technologie Superieure Montreal, Quebec Canada;

    CMC Electronics-Esterline Saint-Laurent, Quebec Canada;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
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