RU98105559A - FREE FORM ORIENTATION SYSTEM - Google Patents

FREE FORM ORIENTATION SYSTEM

Info

Publication number
RU98105559A
RU98105559A RU98105559/28A RU98105559A RU98105559A RU 98105559 A RU98105559 A RU 98105559A RU 98105559/28 A RU98105559/28 A RU 98105559/28A RU 98105559 A RU98105559 A RU 98105559A RU 98105559 A RU98105559 A RU 98105559A
Authority
RU
Russia
Prior art keywords
channel
integrators
block
orientation system
free form
Prior art date
Application number
RU98105559/28A
Other languages
Russian (ru)
Other versions
RU2154810C2 (en
Inventor
Ю.А. Литманович
Original Assignee
Ю.А. Литманович
Filing date
Publication date
Application filed by Ю.А. Литманович filed Critical Ю.А. Литманович
Priority to RU98105559A priority Critical patent/RU2154810C2/en
Priority claimed from RU98105559A external-priority patent/RU2154810C2/en
Publication of RU98105559A publication Critical patent/RU98105559A/en
Application granted granted Critical
Publication of RU2154810C2 publication Critical patent/RU2154810C2/en

Links

Claims (1)

Бесплатформенная система ориентации, включающая трехканальный блок гироскопических датчиков угловой скорости и блок определения угловой ориентации, отличающийся тем, что в состав бесплатформенной системы ориентации включены "n" последовательно соединенных трехканальных интеграторов ("n" не менее 1) и блок синхронного перезапуска интеграторов, при этом выходы трехканального блока датчиков угловой скорости и всех трехканальных интеграторов соединены со входами блока определения угловой ориентации, входы первого трехканального интегратора соединены с одноименными выходами трехканального блока датчиков угловой скорости, а дополнительные входы всех трехканальных интеграторов соединены с выходом блока синхронного перезапуска интеграторов.A strap-on orientation system, including a three-channel block of gyroscopic angular velocity sensors and a block for determining the angular orientation, characterized in that the structure of the strap-on orientation system includes “n” three-channel integrators connected in series (“n” is at least 1) and a synchronous restart unit of integrators, the outputs of the three-channel block of angular velocity sensors and all three-channel integrators are connected to the inputs of the block determining the angular orientation, the inputs of the first three-channel integ the torus is connected to the outputs of the three-channel block of angular velocity sensors of the same name, and the additional inputs of all three-channel integrators are connected to the output of the synchronous restart unit of the integrators.
RU98105559A 1998-03-19 1998-03-19 Gimballess attitude control system RU2154810C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU98105559A RU2154810C2 (en) 1998-03-19 1998-03-19 Gimballess attitude control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU98105559A RU2154810C2 (en) 1998-03-19 1998-03-19 Gimballess attitude control system

Publications (2)

Publication Number Publication Date
RU98105559A true RU98105559A (en) 2000-01-10
RU2154810C2 RU2154810C2 (en) 2000-08-20

Family

ID=20203910

Family Applications (1)

Application Number Title Priority Date Filing Date
RU98105559A RU2154810C2 (en) 1998-03-19 1998-03-19 Gimballess attitude control system

Country Status (1)

Country Link
RU (1) RU2154810C2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2456546C1 (en) * 2010-12-16 2012-07-20 Государственное образовательное учреждение высшего профессионального образования "Тульский государственный университет" (ТулГУ) Strap-down attitude reference system
RU2488774C1 (en) * 2011-12-30 2013-07-27 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Platform-free orbital gyrocompass with arbitrary course orientation of spacecraft

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