A mathematical model of pilot’s heat state adjustment for different flight conditions.

Aviation technics and technology


Аuthors

Pichulin V. S.*, Smirnova G. G.**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: start152295@yandex.ru
**e-mail: galina-ovch@mail.ru

Abstract

The mathematical model worked out in this article provides a way to regulate pilot’s heat state for different flight conditions. Depending on pilots working regime, that is the level of pilot’s expenditure of energy, this model provides a way to determine an optimal temperature of air being forced into ventilation suit and to ensure the comfort pilot’s heat state. This model can be used in individual life support systems.

Keywords:

individual life support systems, ventilation of protective equipment, heat adjustment system, ventilation suit, model of pilot’s heat state.


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