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(19)

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2 697 634

(13)

(51)

IPC

G05D1/00(2006-01-01)

B64C13/00(2006-01-01)

(21) (22)

Application

2017136788, 2017-10-18

(24)

Start date

2017-10-18

(22)

Actual filing date

2017-10-18

(45)

Published

2019-08-15

(72)

Inventor

Popov Aleksandr SergeevichAgeev Andrej MikhajlovichMaltsev Mikhail AleksandrovichMikhajlenko Sergej BorisovichShtankova Nadezhda Viktorovna

(73)

Holder

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

CONTROL METHOD OF MULTISECTIONAL RUDDER OF AIRCRAFT Russian patent published in 2019 - IPC G05D1/00 B64C13/00

Abstract RU 2697634 C2

FIELD: aviation.

SUBSTANCE: invention relates to a method of controlling multi-sectional rudder of an aircraft. To control multi-section rudder, each section control commands are generated to provide required moments. When sections are out of order they are disconnected and fixed in position close to neutral, and section symmetric to it is continued to be used by changing control laws of separate sections.

EFFECT: ensuring maximum stability and controllability of aircraft.

1 cl, 1 dwg

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RU 2 697 634 C2

Authors

Popov Aleksandr Sergeevich

Ageev Andrej Mikhajlovich

Maltsev Mikhail Aleksandrovich

Mikhajlenko Sergej Borisovich

Shtankova Nadezhda Viktorovna

Dates

2019-08-15—Published

2017-10-18—Filed