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Влияние изменений атмосферных условий на результаты оптимизации управления…

Инженерный журнал: наука и инновации

# 1·2017 9

Influence of atmospheric variables on passenger aircraft

control optimization at descent segment

©

T.Yu

. Mozzhorina, E.A. Gubareva

Bauman Moscow State Technical University, Moscow, 105005, Russia

The article considers the

influence of climatic conditions on subsonic long-haul passen-

ger aircraft optimal flight program at descent

segment. F

light program optimization at

this segment takes into account civil aviation operational constraints, namely the vertical

velocity component limitation at descending.

The flight segment descending-braking op-

timization is performed while minimizing the fuel consumption at this flight segment. In

the flight simulation an integrated model of turbojet engine is used, which allows us to

calculate the power plant characteristics at each step of integration of differential equa-

tions. Flight simulation and power plant characteristics are based on modern traditional

approaches. The study considers the climatic conditions influence on the aircraft de-

scending optimal program, carries out calculations for 6 standards of air temperature

changes in height (depending on climate zone). The article examines the atmospheric

conditions influence on the flight program optimization results at the descending seg-

ment.

Keywords:

passenger aircraft control, aircraft control optimization, optimal flight pro-

gram, flight simulation, long-haul passenger aircraft, atmospheric parameters influence,

vertical velocity components, operating limitations.

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