Aircraft landing run control system

Аuthors

Lebedev G. N.^*, Gatich S. A.^**

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

*e-mail: kaf301@mai.ru
**e-mail: s.gatich@yandex.ru

Abstract

The question of aircraft landing run control is considered in the paper. Control is accomplished by the elevator, elerons, rudder, differential brake moment on base wheels and by rotation of front wheel. Control algorithms is described, their efficiency is denoted.

Keywords:

landing; landing run; cornering; rolling resistance

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