JP5528655B2 - 組をなす同一線上の制御モーメントジャイロスコープを制御するための方法及び装置 - Google Patents

組をなす同一線上の制御モーメントジャイロスコープを制御するための方法及び装置 Download PDF

Info

Publication number
JP5528655B2
JP5528655B2 JP2006323060A JP2006323060A JP5528655B2 JP 5528655 B2 JP5528655 B2 JP 5528655B2 JP 2006323060 A JP2006323060 A JP 2006323060A JP 2006323060 A JP2006323060 A JP 2006323060A JP 5528655 B2 JP5528655 B2 JP 5528655B2
Authority
JP
Japan
Prior art keywords
angular momentum
torque
cmgs
spacecraft
cmg
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
JP2006323060A
Other languages
English (en)
Japanese (ja)
Other versions
JP2007163476A (ja
JP2007163476A5 (enExample
Inventor
マイケル・アール・エルガースマ
ダニエル・ピー・ジョンソン
メイソン・エイ・ペック
ブライアン・ケイ・アンダーヒル
ガンター・ステイン
ブレイズ・ジー・モートン
ブライアン・ジェイ・ハミルトン
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.)
Honeywell International Inc
Original Assignee
Honeywell International Inc
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 Honeywell International Inc filed Critical Honeywell International Inc
Publication of JP2007163476A publication Critical patent/JP2007163476A/ja
Publication of JP2007163476A5 publication Critical patent/JP2007163476A5/ja
Application granted granted Critical
Publication of JP5528655B2 publication Critical patent/JP5528655B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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
    • 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
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
JP2006323060A 2005-11-30 2006-11-30 組をなす同一線上の制御モーメントジャイロスコープを制御するための方法及び装置 Active JP5528655B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/291,706 2005-11-30
US11/291,706 US7693619B2 (en) 2005-11-30 2005-11-30 Method and system for controlling sets of collinear control moment gyroscopes with offset determination without attitude trajectory of spacecraft

Publications (3)

Publication Number Publication Date
JP2007163476A JP2007163476A (ja) 2007-06-28
JP2007163476A5 JP2007163476A5 (enExample) 2012-05-17
JP5528655B2 true JP5528655B2 (ja) 2014-06-25

Family

ID=37866159

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2006323060A Active JP5528655B2 (ja) 2005-11-30 2006-11-30 組をなす同一線上の制御モーメントジャイロスコープを制御するための方法及び装置

Country Status (4)

Country Link
US (1) US7693619B2 (enExample)
EP (1) EP1793297B1 (enExample)
JP (1) JP5528655B2 (enExample)
DE (1) DE602006017027D1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101853213B1 (ko) 2016-12-28 2018-04-27 한국항공우주연구원 3개의 관성모멘트 자이로의 김벌 앵글 변경 장치 및 방법

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8209070B2 (en) * 2008-12-17 2012-06-26 Honeywell International Inc. Methods and systems for efficiently orienting an agile vehicle using a gyroscope array
US8014911B2 (en) * 2009-11-03 2011-09-06 Honeywell International Inc. Methods and systems for imposing a momentum boundary while reorienting an agile vehicle with control moment gyroscopes
CN102063521B (zh) * 2010-10-12 2012-07-25 北京理工大学 一种构型可调的单框架控制力矩陀螺群设计方法
US9061775B2 (en) * 2012-06-22 2015-06-23 Isaac M. Ross Method and apparatus for spacecraft attitude control using polynomial interpolation
US8880246B1 (en) * 2012-08-22 2014-11-04 United States Of America As Represented By The Secretary Of The Navy Method and apparatus for determining spacecraft maneuvers
US9567112B1 (en) 2013-06-27 2017-02-14 The United States Of America, As Represented By The Secretary Of The Navy Method and apparatus for singularity avoidance for control moment gyroscope (CMG) systems without using null motion
CN107084744B (zh) * 2017-03-30 2019-12-20 北京航天控制仪器研究所 一种惯性平台系统陀螺仪力矩器系数标定方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4504032A (en) * 1982-03-10 1985-03-12 Rca Corporation Control of nutation in a spacecraft
US6154691A (en) * 1997-09-02 2000-11-28 Honeywell International Inc. Orienting a satellite with controlled momentum gyros
US6039290A (en) * 1998-03-16 2000-03-21 Honeywell Inc. Robust singularity avoidance in satellite attitude control
US6131056A (en) * 1998-03-16 2000-10-10 Honeywell International Inc. Continuous attitude control that avoids CMG array singularities
US6128556A (en) * 1998-03-16 2000-10-03 Honeywell International Inc. CMG control based on angular momentum to control satellite attitude
FR2786283B1 (fr) * 1998-11-19 2001-01-26 Matra Marconi Space France Procede et dispositif de pilotage de l'attitude d'un satellite
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
US6648274B1 (en) * 2002-04-12 2003-11-18 David A. Bailey Virtual reaction wheel array
AU2003294218A1 (en) 2002-08-28 2004-04-23 Arizona Board Of Regents Steering logic for control moment gyro system
US6766227B2 (en) * 2002-11-19 2004-07-20 The Boeing Company Attitude-acquisition methods and systems for controlled spacecraft attitude
US6921049B2 (en) * 2003-11-18 2005-07-26 The Boeing Company System for counteracting a disturbance in a spacecraft
US7246776B2 (en) 2004-07-23 2007-07-24 Honeywell International, Inc. Method and system for CMG array singularity avoidance
US7370833B2 (en) 2005-10-20 2008-05-13 Honeywell International Inc. Method and system for determining a singularity free momentum path

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101853213B1 (ko) 2016-12-28 2018-04-27 한국항공우주연구원 3개의 관성모멘트 자이로의 김벌 앵글 변경 장치 및 방법

Also Published As

Publication number Publication date
JP2007163476A (ja) 2007-06-28
DE602006017027D1 (de) 2010-11-04
EP1793297A3 (en) 2008-09-10
US20070124032A1 (en) 2007-05-31
EP1793297A2 (en) 2007-06-06
EP1793297B1 (en) 2010-09-22
US7693619B2 (en) 2010-04-06

Similar Documents

Publication Publication Date Title
JP4307247B2 (ja) ジャイロダインのクラスターによって人工衛星の姿勢を制御しかつ操舵するための方法及び装置
US6917862B2 (en) Singularity escape/avoidance steering logic for control moment gyro systems
EP1908686B1 (en) Hierarchial strategy for singularity avoidance in arrays of control moment gyroscopes
JP2004535324A5 (enExample)
US6154691A (en) Orienting a satellite with controlled momentum gyros
CN108627158B (zh) 使卫星的命令动态最小化的方法和设备
Kasai et al. Spacecraft attitude maneuver using two single-gimbal control moment gyros
JP5528655B2 (ja) 組をなす同一線上の制御モーメントジャイロスコープを制御するための方法及び装置
Valk et al. Directional singularity escape and avoidance for single-gimbal control moment gyroscopes
JP4783366B2 (ja) Ｃｍｇアレイにおけるトルクを最適化するための方法及びシステム
Kojima Singularity analysis and steering control laws for adaptive-skew pyramid-type control moment gyros
JP4630332B2 (ja) Ｃｍｇアレイ特異性回避のための方法及びシステム
JP5221021B2 (ja) 特異点の無い運動量経路を決定する方法及び装置
EP1749743B1 (en) A method and system for determining a singularity free momentum path
Guo et al. Pyramid-type single-gimbal control moment gyro system singularity avoidance using gimbal reorientation
JP2023151835A (ja) 姿勢制御システム、姿勢制御方法、および、姿勢制御プログラム
Elliott et al. Optimal solution for torque capability of control moment gyroscopes
JP5052852B2 (ja) 特異点のない運動量経路を決定するための方法およびシステム
Zeledon et al. Singularity-Free constrained steering law for triplet control moment gyros
Kanzawa et al. Attitude Maneuver Tests Using CMGs Mounted in a Three-Axis Free Dynamics Simulator
權相元 Attitude Control of Small Satellites Using Single-Gimbal Control Moment Gyros

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20090826

RD04 Notification of resignation of power of attorney

Free format text: JAPANESE INTERMEDIATE CODE: A7424

Effective date: 20110913

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20120327

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20120613

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20120911

A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20130801

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20131202

A911 Transfer to examiner for re-examination before appeal (zenchi)

Free format text: JAPANESE INTERMEDIATE CODE: A911

Effective date: 20140115

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20140320

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20140416

R150 Certificate of patent or registration of utility model

Ref document number: 5528655

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250