SU1839928A1 - Electromechanical actuating member for spacecraft orientation and stabilization system - Google Patents

Electromechanical actuating member for spacecraft orientation and stabilization system

Info

Publication number
SU1839928A1
SU1839928A1 SU2274223/11A SU2274223A SU1839928A1 SU 1839928 A1 SU1839928 A1 SU 1839928A1 SU 2274223/11 A SU2274223/11 A SU 2274223/11A SU 2274223 A SU2274223 A SU 2274223A SU 1839928 A1 SU1839928 A1 SU 1839928A1
Authority
SU
USSR - Soviet Union
Prior art keywords
actuating member
flywheel
electromechanical actuating
stabilization system
motor
Prior art date
Application number
SU2274223/11A
Other languages
Russian (ru)
Inventor
Юрий Иванович Юрьев
Герман Николаевич Гладышев
Виктор Степанович Дмитриев
Original Assignee
Государственное научно-производственное предприятие "Полюс"
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 научно-производственное предприятие "Полюс" filed Critical Государственное научно-производственное предприятие "Полюс"
Priority to SU2274223/11A priority Critical patent/SU1839928A1/en
Application granted granted Critical
Publication of SU1839928A1 publication Critical patent/SU1839928A1/en

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Landscapes

  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

FIELD: spacecraft equipment.SUBSTANCE: proposed electromechanical actuating member has body, electric motor with flywheel, tachogenerator and control unit for control of precision motion of motor-flywheel connected with two torque sensors. Body is spherical and form and is provided with three intersecting circular grooves. Motor-flywheel is mounted in body by means of trunnions. Retainers electrically connected with control unit are mounted in point of intersection of body grooves.EFFECT: reduced mass and overall dimensions.5 dwg
SU2274223/11A 1980-03-07 1980-03-07 Electromechanical actuating member for spacecraft orientation and stabilization system SU1839928A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2274223/11A SU1839928A1 (en) 1980-03-07 1980-03-07 Electromechanical actuating member for spacecraft orientation and stabilization system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2274223/11A SU1839928A1 (en) 1980-03-07 1980-03-07 Electromechanical actuating member for spacecraft orientation and stabilization system

Publications (1)

Publication Number Publication Date
SU1839928A1 true SU1839928A1 (en) 2006-06-20

Family

ID=60541553

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2274223/11A SU1839928A1 (en) 1980-03-07 1980-03-07 Electromechanical actuating member for spacecraft orientation and stabilization system

Country Status (1)

Country Link
SU (1) SU1839928A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2555080C2 (en) * 2008-10-31 2015-07-10 Таль Method and system to rule out saturation of spacecraft inertial wheels
EA028853B1 (en) * 2015-07-07 2018-01-31 федеральное государственное автономное образовательное учреждение высшего образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет)" (СГАУ) Method of spatial reorientation and change of parameters of spacecraft angular motion

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2555080C2 (en) * 2008-10-31 2015-07-10 Таль Method and system to rule out saturation of spacecraft inertial wheels
EA028853B1 (en) * 2015-07-07 2018-01-31 федеральное государственное автономное образовательное учреждение высшего образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет)" (СГАУ) Method of spatial reorientation and change of parameters of spacecraft angular motion

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