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2 168 704

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C1

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IPC

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Application

2000101741/28, 2000-01-27

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Start date

2000-01-27

(22)

Actual filing date

2000-01-27

(45)

Published

2001-06-10

(72)

Inventor

Dzhandzhgava G.I.Kavinskij V.V.Negrikov V.V.Orekhov M.I.Semash A.A.Shkred V.K.

(73)

Holder

Otkrytoe Aktsionernoe Obshchestvo Ramenskoe Priborostroitel'Noe Konstruktorskoe Bjuro

COMPLEX NAVIGATIONAL SYSTEM Russian patent published in 2001 - IPC

Abstract RU 2168704 C1

FIELD: aircraft instrument engineering, applicable as a component of the on-board equipment of flight vehicles for solution of the problems of guidance, aiming and use of combat facilities. SUBSTANCE: the system has an inertial velocity and heading sensor, correcting filter, satellite velocity and coordinate transducer, as well as a navigation parameters formation unit. In addition the system has a memory unit and a compass bearing error formation unit connected between the above inertial sensor and the filter. These units enhance the accuracy of the system heading and velocity components characteristics. EFFECT: enhanced combat efficiency of employment of flight vehicles equipped by the claimed complex system. 1 dwg

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RU 2 168 704 C1

Authors

Dzhandzhgava G.I.

Kavinskij V.V.

Negrikov V.V.

Orekhov M.I.

Semash A.A.

Shkred V.K.

Dates

2001-06-10—Published

2000-01-27—Filed

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