DE602007008934D1 - Steuermomentkreisel und vorrichtung zu seiner montage - Google Patents

Steuermomentkreisel und vorrichtung zu seiner montage

Info

Publication number
DE602007008934D1
DE602007008934D1 DE602007008934T DE602007008934T DE602007008934D1 DE 602007008934 D1 DE602007008934 D1 DE 602007008934D1 DE 602007008934 T DE602007008934 T DE 602007008934T DE 602007008934 T DE602007008934 T DE 602007008934T DE 602007008934 D1 DE602007008934 D1 DE 602007008934D1
Authority
DE
Germany
Prior art keywords
stator
assembly
chock
rotor
axis
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
DE602007008934T
Other languages
English (en)
Inventor
Philippe Faucheux
Stephane Chupin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space SAS
Original Assignee
Astrium SAS
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 Astrium SAS filed Critical Astrium SAS
Publication of DE602007008934D1 publication Critical patent/DE602007008934D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C17/00—Aircraft stabilisation not otherwise provided for
    • B64C17/02—Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus
    • B64C17/06—Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus by gyroscopic apparatus
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/12—Gyroscopes
    • Y10T74/1282—Gyroscopes with rotor drive

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Gyroscopes (AREA)
  • Electromechanical Clocks (AREA)
  • Accessories Of Cameras (AREA)
  • Medicines Containing Material From Animals Or Micro-Organisms (AREA)
  • Vibration Prevention Devices (AREA)
  • Telephone Function (AREA)
  • Apparatuses For Generation Of Mechanical Vibrations (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Coupling Device And Connection With Printed Circuit (AREA)
  • Vehicle Body Suspensions (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
DE602007008934T 2006-10-23 2007-10-03 Steuermomentkreisel und vorrichtung zu seiner montage Active DE602007008934D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0609278A FR2907423B1 (fr) 2006-10-23 2006-10-23 Gyrodyne et son dispositif de montage
PCT/FR2007/052066 WO2008050019A2 (fr) 2006-10-23 2007-10-03 Gyrodyne et son dispositif de montage

Publications (1)

Publication Number Publication Date
DE602007008934D1 true DE602007008934D1 (de) 2010-10-14

Family

ID=38038633

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007008934T Active DE602007008934D1 (de) 2006-10-23 2007-10-03 Steuermomentkreisel und vorrichtung zu seiner montage

Country Status (10)

Country Link
US (1) US8052093B2 (de)
EP (1) EP2081829B1 (de)
JP (1) JP5095746B2 (de)
KR (1) KR101441628B1 (de)
AT (1) ATE479600T1 (de)
DE (1) DE602007008934D1 (de)
ES (1) ES2349830T3 (de)
FR (1) FR2907423B1 (de)
IL (1) IL198340A (de)
WO (1) WO2008050019A2 (de)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8371534B1 (en) * 2007-09-14 2013-02-12 Lockheed Martin Corporation System for isolating vibration among a plurality of instruments
US8312782B2 (en) * 2009-06-18 2012-11-20 Honeywell International Inc. Control moment gyroscope based momentum control systems in small satellites
US20120097798A1 (en) * 2010-10-25 2012-04-26 Rust Sr John H Inertial mass suspension
US8672062B2 (en) 2011-05-26 2014-03-18 Gregory C Schroll Internal means for rotating an object between gravitationally stable states
KR101372807B1 (ko) * 2012-07-25 2014-03-12 한국항공우주연구원 3차원 구체 구동시스템
CN102901492B (zh) * 2012-09-29 2015-04-22 北京控制工程研究所 一种机电一体化小型变速控制力矩陀螺
KR101474274B1 (ko) * 2013-03-25 2014-12-18 한국항공우주연구원 제어 모멘트 자이로
US10326914B2 (en) * 2013-08-12 2019-06-18 Sun Chemical Corporation Method for digitally printing color selection cards by matching the base inks to the base paints, dyes, or plastics
KR101384135B1 (ko) * 2013-12-06 2014-04-17 한국항공우주연구원 비접착식 진동저감장치
CN105000201B (zh) * 2015-07-21 2017-09-29 上海新跃仪表厂 一种五棱锥控制力矩陀螺群隔振支架一体化装置
FR3041327B1 (fr) * 2015-09-18 2019-05-31 Thales Actionneur gyroscopique a double guidage cardan, element de suspension et element de butee
CN105468871B (zh) * 2015-12-23 2018-09-18 北京控制工程研究所 一种动量轮成功包络分析与应用方法
US10228248B2 (en) 2016-02-02 2019-03-12 The Boeing Company Hybrid power source and control moment gyroscope
US10472098B2 (en) * 2016-10-25 2019-11-12 Honeywell International Inc. Mass efficient reaction wheel assembly systems including multi-faceted bracket structures
KR101796541B1 (ko) * 2017-03-29 2017-12-01 (주)나라스페이스테크놀로지 제어 모멘트 자이로스코프 및 이를 포함하는 소형 인공위성
US12092459B2 (en) * 2018-03-28 2024-09-17 Verton IP Pty Ltd Arrangements for rotational apparatus
CN109466807B (zh) * 2018-12-13 2020-07-14 中国空间技术研究院 适用于高轨卫星通用锥杆捕获机构的滚珠式导向阻尼机构
CN109732338B (zh) * 2018-12-29 2020-08-25 北京发那科机电有限公司 一种指尖陀螺装配系统和装配方法
EP3705408A1 (de) * 2019-03-08 2020-09-09 Veoware SPRL Modulares und konfigurierbares lagesteuerungssystem für ein raumfahrzeug
KR102188740B1 (ko) 2019-12-04 2020-12-08 한국항공대학교산학협력단 가변 속도 제어 모멘트 자이로스코프 장치
CN110888444B (zh) * 2019-12-04 2021-03-09 腾讯科技（深圳）有限公司 自平衡行驶装置及其控制方法
CN112039244B (zh) * 2020-08-12 2021-09-07 北京控制工程研究所 一种精密支承的控制力矩陀螺框架转子组件及装配方法
KR102638917B1 (ko) * 2021-08-30 2024-02-21 주식회사 엠앤씨솔루션 제어 모멘트 자이로
CN113998160B (zh) * 2021-11-10 2024-04-19 中国科学院长春光学精密机械与物理研究所 集成重力卸载机构

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3340739A (en) * 1967-09-12 Jr., etal segmented gimbals
US3446080A (en) * 1965-10-23 1969-05-27 Clary Corp Method and means for reducing gyro gimbal bearing friction
US3452948A (en) * 1967-01-03 1969-07-01 Garrett Corp System and method for free body stabilization and orientation
US4275861A (en) * 1978-08-04 1981-06-30 Rca Corporation Orientation of momentum stabilized vehicles
FR2602045B1 (fr) * 1986-07-25 1988-12-02 Sfena Horizon gyroscopique
US5112012A (en) * 1989-10-26 1992-05-12 Yuan Mark S Tilting momentum wheel for spacecraft
US5368271A (en) * 1992-03-02 1994-11-29 Hughes Aircraft Company Gimbal vibration isolation system
JPH06132716A (ja) * 1992-10-19 1994-05-13 Furuno Electric Co Ltd アンテナ姿勢制御装置
US5820079A (en) * 1994-04-05 1998-10-13 Hughes Electronics Mechanism for mounting and actuating a momentum wheel with high vibration isolation
JPH08247766A (ja) * 1995-03-10 1996-09-27 Japan Aviation Electron Ind Ltd レートジャイロ
US5820078A (en) * 1996-09-27 1998-10-13 Hughes Electronics Corporation Control motion gyro with vibration isolation
US5971375A (en) * 1996-11-26 1999-10-26 Trw Inc. Isolator apparatus for multi-dimensional vibrational disturbances
FR2773775B1 (fr) * 1998-01-20 2000-03-24 Matra Marconi Space France Actionneur gyroscopique
US6135392A (en) * 1998-09-29 2000-10-24 Hughes Electronics Corporation Spacecraft attitude control actuator and method
FR2786283B1 (fr) 1998-11-19 2001-01-26 Matra Marconi Space France Procede et dispositif de pilotage de l'attitude d'un satellite
US6515221B1 (en) * 2000-08-01 2003-02-04 Honeywell International Inc. Modular reaction wheel assembly to shield electronics on a satellite
JP2002286451A (ja) * 2001-03-27 2002-10-03 Tokimec Inc ジャイロコンパス用防振緩衝装置
FR2826470B1 (fr) 2001-06-26 2003-09-19 Astrium Sas Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes
FR2837580B1 (fr) * 2002-03-21 2005-06-03 Astrium Sas Actionneur gyroscopique de pilotage de l'attitude d'un vehicule spatial

Also Published As

Publication number Publication date
EP2081829A2 (de) 2009-07-29
JP2010507793A (ja) 2010-03-11
JP5095746B2 (ja) 2012-12-12
WO2008050019A3 (fr) 2008-07-17
FR2907423A1 (fr) 2008-04-25
WO2008050019A2 (fr) 2008-05-02
US8052093B2 (en) 2011-11-08
KR101441628B1 (ko) 2014-09-22
FR2907423B1 (fr) 2009-07-03
KR20090116690A (ko) 2009-11-11
ES2349830T8 (es) 2011-03-18
ATE479600T1 (de) 2010-09-15
IL198340A (en) 2012-05-31
US20100006705A1 (en) 2010-01-14
EP2081829B1 (de) 2010-09-01
ES2349830T3 (es) 2011-01-11
IL198340A0 (en) 2010-02-17

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