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2 520 872

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IPC

G01S13/00(2006-01-01)

G05D1/10(2006-01-01)

G05D1/08(2006-01-01)

G01C21/06(2006-01-01)

B64D45/04(2006-01-01)

(21) (22)

Application

2012129081/11, 2012-07-10

(24)

Start date

2012-07-10

(22)

Actual filing date

2012-07-10

(45)

Published

2014-06-27

(72)

Inventor

Beljaev Mikhail AleksandrovichGushchin Grigorij MikhajlovichKabakov Vladimir BorisovichKavinskij Vladimir ValentinovichLytkin Pavel DmitrievichNikulin Aleksandr StepanovichNikulina Anna AleksandrovnaObolenskij Jurij Gennad'EvichSemash Aleksandr AleksandrovichShukajlo Aleksej Viktorovich

(73)

Holder

Otkrytoe Aktsionernoe Obshchestvo Priborostroitel'Noe Konstruktorskoe Bjuro"Otkrytoe Aktsionernoe Obshchestvo Samoletostroitel'Naja Korporatsija

COMPLEX SYSTEM FOR CONTROLLING AIRCRAFT TRAJECTORY DURING APPROACH LANDING Russian patent published in 2014 - IPC G01S13/00 G05D1/10 G05D1/08 G01C21/06 B64D45/04

Abstract RU 2520872 C2

FIELD: physics; control.

SUBSTANCE: invention relates to a complex system for controlling aircraft trajectory during approach landing. The system comprises an inertial navigation system, an air signal system, a landing signal indicator, a complex information processing unit, a satellite navigation system, a memory unit, a landing strip parameter determining unit, a virtual heading-glide beacon location unit, a unit for determining the direction and range of the virtual heading-glide beacon, first and second adders and a unit for determining the elevation angle of the virtual heading-glide beacon.

EFFECT: high reliability and safety of landing aircraft.

7 dwg

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RU 2 520 872 C2

Authors

Beljaev Mikhail Aleksandrovich

Gushchin Grigorij Mikhajlovich

Kabakov Vladimir Borisovich

Kavinskij Vladimir Valentinovich

Lytkin Pavel Dmitrievich

Nikulin Aleksandr Stepanovich

Nikulina Anna Aleksandrovna

Obolenskij Jurij Gennad'Evich

Semash Aleksandr Aleksandrovich

Shukajlo Aleksej Viktorovich

Dates

2014-06-27—Published

2012-07-10—Filed