Analysis of aircraft control system and moment of inertia characteristics in case of variable payload and fuel masses.

Aviation technics and technology


Аuthors

Dolgov O. S.

,

e-mail: dolgov@mai.ru

Abstract

The paper describes new approaches of moment of inertia shape formation of future technology vehicle. Defined preferable zones of placing fuel and payload accordingly its mass. The analysis features of the definition of moment-inertia characteristics of the aircraft relative to the axes OX, OZ and OY. The aspects of the harmonization of moment-inertia shape the possibilities of governance. Analyzed features of aircraft moment-inertia characteristics over axes OX, OZ and OY formation. Identified the aspects of adapting moment-inertia shape formation with the possibilities of aircraft control system.

Keywords:

moment of inertia, fuel tanks, payload, layout, control system


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