Adapting of control system parameters with moment of inertia characteristics of the aircraft in case of variable payload mass and fuel output.
Aviation technics and technology
Аuthors
*, **, ***Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
*e-mail: dolgov@mai.ru
**e-mail: nkuprikov@gmail.com
***e-mail: maximmai@mail.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. Rated regularities between the geometric characteristics of alternative variants of placing fuel in the wing and payload in the fuselage and the moment of inertia parameters of the aircraft. Designed method of moment inertia characteristics of long-haul passenger aircraft determination with targeted accurate intervals.Keywords:
moment of inertia; fuel tank layout; payload layout, control systemDownload