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2 600 025

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(51)

IPC

G05D1/08(2006-01-01)

B64C19/00(2006-01-01)

(21) (22)

Application

2014142715/11, 2014-10-22

(24)

Start date

2014-10-22

(22)

Actual filing date

2014-10-22

(45)

Published

2016-10-20

(72)

Inventor

Vereshshikov Dmitrij ViktorovichKostin Pavel SergeevichVereshshagin Yurij OlegovichMakarov Ilya KonstantinovichKuznetsov Aleksandr Dmitrievich

(73)

Holder

Federalnoe Gosudarstvennoe Kazennoe Voennoe Obrazovatelnoe Uchrezhdenie Vysshego Professionalnogo Obrazovaniya Uchebno-Nauchnyj Tsentr Voenno-Vozdushnykh Sil Akademiya Imeni Professora N.E. Zhukovskogo I Yu.A. Gagarina" Voronezh) Ministerstva Oborony Rossijskoj Federatsii

METHOD FOR ADAPTIVE ROLL CONTROL OF AIRCRAFT Russian patent published in 2016 - IPC G05D1/08 B64C19/00

Abstract RU 2600025 C2

FIELD: aviation.

SUBSTANCE: invention relates to a method of adaptive roll control of aircraft. For adaptive roll control of aircraft, method comprises estimating current aerodynamic parameters of transverse motion of aircraft, generating control signals monitoring change of quantity and arrangement of external suspensions compared with initial arrangement, calculating axial and centrifugal moments of inertia of aircraft adjusting aircraft control commands.

EFFECT: higher stability and controllability of transverse motion of aircraft.

1 cl, 1 dwg

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RU 2 600 025 C2

Authors

Vereshshikov Dmitrij Viktorovich

Kostin Pavel Sergeevich

Vereshshagin Yurij Olegovich

Makarov Ilya Konstantinovich

Kuznetsov Aleksandr Dmitrievich

Dates

2016-10-20—Published

2014-10-22—Filed