JP2007163476A5 - - Google Patents

Download PDF

Info

Publication number
JP2007163476A5
JP2007163476A5 JP2006323060A JP2006323060A JP2007163476A5 JP 2007163476 A5 JP2007163476 A5 JP 2007163476A5 JP 2006323060 A JP2006323060 A JP 2006323060A JP 2006323060 A JP2006323060 A JP 2006323060A JP 2007163476 A5 JP2007163476 A5 JP 2007163476A5
Authority
JP
Japan
Prior art keywords
defects
mentioned
desirable
handles
pat
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.)
Granted
Application number
JP2006323060A
Other languages
English (en)
Japanese (ja)
Other versions
JP2007163476A (ja
JP5528655B2 (ja
Filing date
Publication date
Priority claimed from US11/291,706 external-priority patent/US7693619B2/en
Application filed filed Critical
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

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 true JP2007163476A5 (enExample) 2012-05-17
JP5528655B2 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)

Families Citing this family (8)

* 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
KR101853213B1 (ko) 2016-12-28 2018-04-27 한국항공우주연구원 3개의 관성모멘트 자이로의 김벌 앵글 변경 장치 및 방법
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

Similar Documents

Publication Publication Date Title
EP1866868A4 (en) Album generating apparatus, album generating method and program
EP1866869A4 (en) Album generating apparatus, album generating method and program
EP2013845A4 (en) SYSTEM FOR AN ONLINE CONTENT MARKETPLACE AND OPERATING METHOD THEREFOR
CL2007003274A1 (es) Un metodo para tomar muestras de semilla, que comprende posicionar automaticamente la semilla en una orientacion predeterminada, retirar una muestra mensurable proveniente de la semilla; y aparato para tomar muestras de una o mas semilla.
EP2151230A4 (en) OIL-IN-WATER EMULSION COMPOSITION AND METHOD FOR PREPARING THE SAME
IL191556A0 (en) Solar system and method for the operation thereof
EP1943094A4 (en) DEVICE AND METHOD FOR PRODUCING FULL-NANNY-TENDER FORESTS, THREADS AND COMPOSITE STRUCTURES
EP2014375A4 (en) FAULT REPAIR DEVICE, FAULT REPAIR METHOD, PROGRAM, AND COMPUTER READABLE RECORDING MEDIUM
EP2002473A4 (en) PUNCH TESTING DEVICE AND PUNCH TEST PROCEDURE THEREWITH
TWI351224B (en) Cursor controlling method and apparatus using the same
TWI370504B (en) Electrostatic chuck, substrate processing apparatus having the same, and substrate processing method using the same
GB2419852B (en) Scribing apparatus, substrate cutting apparatus equipped with the scribing apparatus, and substrate cutting method using the substrate cutting apparatus
NO20053230L (no) Sikt- og fluidseparasjonsapparat samt fremgangsmate ved bruk av samme.
JP2007163476A5 (enExample)
SG129313A1 (en) Carbon black, method for producing the same, and its use
EP1949939A4 (en) PRESSURE DRIVE APPARATUS AND METHOD FOR CONTROLLING THE SAME
BRPI0720420A2 (pt) Método e aparelho de processamento de vídeo, programa de processamento de vídeo e meio de armazenamento que armazena o programa
WO2009019248A3 (de) Verfahren zum erzeugen eines templates
TWI367457B (en) Image processing method and apparatus, image processing program, and storage medium for storing the program
PL1816101T3 (pl) ­­­­Piec przemysłowy z urządzeniem do reformingu parowego i stosujący go sposób reformingu parowego
NL2000985A1 (nl) Werkwijze en inrichting voor het verkleinen van de verschillen tussen de trekspanningen in flexibele elementen.
EP1845720A4 (en) PROGRAM RECORDING DEVICE, PROGRAM RECORDING PROCEDURE, PROGRAM RECOGNITION PROGRAM AND COMPUTER READABLE RECORDING MEDIUM
EP1926101A4 (en) MEDIA SERVER, CONTROL PROCEDURE FOR A MEDIA SERVER AND PROGRAM
GB2433724B (en) Printing device and printing method using the same
WO2010039810A3 (en) Solute stabilization of sheets formed from a melt