SU1840258A1 - Inertial navigation system - Google Patents

Inertial navigation system

Info

Publication number
SU1840258A1
SU1840258A1 SU3146767/28A SU3146767A SU1840258A1 SU 1840258 A1 SU1840258 A1 SU 1840258A1 SU 3146767/28 A SU3146767/28 A SU 3146767/28A SU 3146767 A SU3146767 A SU 3146767A SU 1840258 A1 SU1840258 A1 SU 1840258A1
Authority
SU
USSR - Soviet Union
Prior art keywords
unit
generation
angular orientation
orientation matrix
movable
Prior art date
Application number
SU3146767/28A
Other languages
Russian (ru)
Inventor
Валерий Залманович Гусинский
Владимир Михайлович Лесючевский
Юрий Аронович Литманович
Виктор Александрович Шапиро
Original Assignee
Государственное унитарное предприятие "Центральный научно-исследовательский институт "Электроприбор"
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Государственное унитарное предприятие "Центральный научно-исследовательский институт "Электроприбор" filed Critical Государственное унитарное предприятие "Центральный научно-исследовательский институт "Электроприбор"
Priority to SU3146767/28A priority Critical patent/SU1840258A1/en
Application granted granted Critical
Publication of SU1840258A1 publication Critical patent/SU1840258A1/en

Links

Abstract

FIELD: navigational gyroscopic devices, applicable in high-precision navigation complexes of movable objects, in particular, in naval ones.SUBSTANCE: the system has a unit of three accelerometers with orthogonal sensitivity axes, the unit is rigidly mounted on the movable object, and a unit for determination of the angular orientation matrix of the movable object. Besides, the system, additionally uses n series-connected three-channel integrators, selector of time operation mode of the three-channel integrators, unit for computation of the derivatives of the angular orientation matrix, unit for generation of travel increments, unit for generation of the object co-ordinates and velocities.EFFECT: provided required precision in the condition of vibration action on the object.1 dwg
SU3146767/28A 1986-06-27 1986-06-27 Inertial navigation system SU1840258A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3146767/28A SU1840258A1 (en) 1986-06-27 1986-06-27 Inertial navigation system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3146767/28A SU1840258A1 (en) 1986-06-27 1986-06-27 Inertial navigation system

Publications (1)

Publication Number Publication Date
SU1840258A1 true SU1840258A1 (en) 2006-09-10

Family

ID=60537696

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3146767/28A SU1840258A1 (en) 1986-06-27 1986-06-27 Inertial navigation system

Country Status (1)

Country Link
SU (1) SU1840258A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2491507C1 (en) * 2011-12-29 2013-08-27 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Meter of angular position of item
RU2539846C1 (en) * 2013-10-18 2015-01-27 Открытое акционерное общество "Научно-исследовательский институт телевидения" Inertial radio navigation system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2491507C1 (en) * 2011-12-29 2013-08-27 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Meter of angular position of item
RU2539846C1 (en) * 2013-10-18 2015-01-27 Открытое акционерное общество "Научно-исследовательский институт телевидения" Inertial radio navigation system

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