SG11201609732SA - Control moment gyroscope module for satellites - Google Patents

Control moment gyroscope module for satellites

Info

Publication number
SG11201609732SA
SG11201609732SA SG11201609732SA SG11201609732SA SG11201609732SA SG 11201609732S A SG11201609732S A SG 11201609732SA SG 11201609732S A SG11201609732S A SG 11201609732SA SG 11201609732S A SG11201609732S A SG 11201609732SA SG 11201609732S A SG11201609732S A SG 11201609732SA
Authority
SG
Singapore
Prior art keywords
satellites
control moment
moment gyroscope
gyroscope module
module
Prior art date
Application number
SG11201609732SA
Inventor
Moses James Goh
Robert Devasahayam
Original Assignee
St Electronics Satcom & Sensor Systems Pte Ltd
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 St Electronics Satcom & Sensor Systems Pte Ltd filed Critical St Electronics Satcom & Sensor Systems Pte Ltd
Priority to SG11201609732SA priority Critical patent/SG11201609732SA/en
Publication of SG11201609732SA publication Critical patent/SG11201609732SA/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02—Rotary gyroscopes
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02—Rotary gyroscopes
    • G01C19/04—Details
SG11201609732SA 2014-06-11 2014-11-03 Control moment gyroscope module for satellites SG11201609732SA (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SG11201609732SA SG11201609732SA (en) 2014-06-11 2014-11-03 Control moment gyroscope module for satellites

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SG10201403151S 2014-06-11
PCT/SG2014/000514 WO2015190996A1 (en) 2014-06-11 2014-11-03 Control moment gyroscope module for satellites
SG11201609732SA SG11201609732SA (en) 2014-06-11 2014-11-03 Control moment gyroscope module for satellites

Publications (1)

Publication Number Publication Date
SG11201609732SA true SG11201609732SA (en) 2016-12-29

Family

ID=54833960

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11201609732SA SG11201609732SA (en) 2014-06-11 2014-11-03 Control moment gyroscope module for satellites

Country Status (5)

Country Link
US (1) US10086958B2 (en)
EP (1) EP3154861B1 (en)
KR (1) KR101929966B1 (en)
SG (1) SG11201609732SA (en)
WO (1) WO2015190996A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3511253A4 (en) * 2016-09-09 2019-09-11 Mitsubishi Electric Corporation Posture control device, posture control system, ground station, artificial satellite, method for controlling posture, and program
KR102158310B1 (en) * 2018-07-17 2020-09-21 세종대학교산학협력단 Self balancing carrier robot testing unit
CN110502024B (en) * 2019-07-23 2020-10-20 北京控制工程研究所 Quasi-universal attitude executing mechanism based on space parallel mechanism
CN112039244B (en) * 2020-08-12 2021-09-07 北京控制工程研究所 Control moment gyro frame rotor assembly of precise support and assembling method

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3105657A (en) * 1961-07-13 1963-10-01 Mueller Fritz Kurt Spherical-flywheel attitude-control system
GB8327436D0 (en) * 1983-10-13 1983-12-07 British Aerospace Gyroscopes
WO2000005549A1 (en) * 1998-07-23 2000-02-03 Bristol Aerospace Limited System and method for spacecraft attitude control
US7290737B2 (en) * 2005-09-29 2007-11-06 United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Nonsurvivable momentum exchange system
US8127631B2 (en) * 2008-09-17 2012-03-06 Honeywell International Inc. Rotor assembly including strain relief feature
US8312782B2 (en) * 2009-06-18 2012-11-20 Honeywell International Inc. Control moment gyroscope based momentum control systems in small satellites
US8596151B2 (en) * 2010-02-26 2013-12-03 Honeywell International Inc. Momentum exchange assemblies and inner gimbal assemblies for use in control moment gyroscopes
US9354079B2 (en) * 2012-05-21 2016-05-31 Honeywell International Inc. Control moment gyroscopes including torsionally-stiff spoked rotors and methods for the manufacture thereof

Also Published As

Publication number Publication date
WO2015190996A1 (en) 2015-12-17
KR20160149307A (en) 2016-12-27
EP3154861A1 (en) 2017-04-19
KR101929966B1 (en) 2018-12-17
EP3154861A4 (en) 2018-01-17
US10086958B2 (en) 2018-10-02
US20170121037A1 (en) 2017-05-04
EP3154861B1 (en) 2020-04-22

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