JP2002506774A5 - - Google Patents
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- JP2002506774A5 JP2002506774A5 JP2000536623A JP2000536623A JP2002506774A5 JP 2002506774 A5 JP2002506774 A5 JP 2002506774A5 JP 2000536623 A JP2000536623 A JP 2000536623A JP 2000536623 A JP2000536623 A JP 2000536623A JP 2002506774 A5 JP2002506774 A5 JP 2002506774A5
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- JP
- Japan
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Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/042,515 US6128556A (en) | 1998-03-16 | 1998-03-16 | CMG control based on angular momentum to control satellite attitude |
| US09/042,515 | 1998-03-16 | ||
| PCT/US1999/005703 WO1999047420A1 (en) | 1998-03-16 | 1999-03-15 | Cmg control based on angular momentum to control satellite attitude |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2002506774A JP2002506774A (ja) | 2002-03-05 |
| JP2002506774A5 true JP2002506774A5 (ja) | 2006-04-27 |
| JP4249901B2 JP4249901B2 (ja) | 2009-04-08 |
Family
ID=21922348
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2000536623A Expired - Fee Related JP4249901B2 (ja) | 1998-03-16 | 1999-03-15 | 衛星の姿勢制御のための各運動量に基づくｃｍｇ制御 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6128556A (ja) |
| EP (1) | EP1064197B1 (ja) |
| JP (1) | JP4249901B2 (ja) |
| DE (1) | DE69927005T2 (ja) |
| WO (1) | WO1999047420A1 (ja) |
Families Citing this family (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6729580B2 (en) | 2001-04-05 | 2004-05-04 | Northrop Grumman Corporation | Method and system for directing an object using gyroscopes |
| US6891498B2 (en) | 2002-03-28 | 2005-05-10 | Honeywell International Inc. | Inertial reference system for a spacecraft |
| US6682019B2 (en) | 2002-04-04 | 2004-01-27 | Honeywell International Inc. | Minimum energy wheel configurations for energy storage and attitude control |
| US6648274B1 (en) | 2002-04-12 | 2003-11-18 | David A. Bailey | Virtual reaction wheel array |
| US6917862B2 (en) * | 2002-08-28 | 2005-07-12 | Arizona Board Of Regents | Singularity escape/avoidance steering logic for control moment gyro systems |
| US7561947B2 (en) * | 2003-10-06 | 2009-07-14 | Honeywell International Inc. | Dynamic CMG array and method |
| US7246776B2 (en) * | 2004-07-23 | 2007-07-24 | Honeywell International, Inc. | Method and system for CMG array singularity avoidance |
| US7014150B2 (en) * | 2004-07-30 | 2006-03-21 | Honeywell International Inc. | Method and system for optimizing torque in a CMG array |
| JP4511390B2 (ja) * | 2005-03-01 | 2010-07-28 | 三菱電機株式会社 | 人工衛星の姿勢制御装置 |
| US7370833B2 (en) * | 2005-10-20 | 2008-05-13 | Honeywell International Inc. | Method and system for determining a singularity free momentum path |
| US7693619B2 (en) * | 2005-11-30 | 2010-04-06 | Honeywell International Inc. | Method and system for controlling sets of collinear control moment gyroscopes with offset determination without attitude trajectory of spacecraft |
| US7805226B2 (en) * | 2006-09-29 | 2010-09-28 | Honeywell International Inc. | Hierarchical strategy for singularity avoidance in arrays of control moment gyroscopes |
| JP5126107B2 (ja) * | 2009-02-19 | 2013-01-23 | 三菱電機株式会社 | 人工衛星の姿勢制御装置 |
| 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 |
| 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 |
| KR101517391B1 (ko) * | 2013-12-27 | 2015-05-06 | 한국항공우주연구원 | 단일 입출력 제어기를 이용한 인공위성의 3축 자세 제어 시스템 |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3606636C1 (de) * | 1986-02-28 | 1987-11-05 | Messerschmitt Boelkow Blohm | Verfahren zur Bestimmung von Erdmagnetfeldkomponenten bezueglich eines satellitenfesten Koordinatensystems |
| US4949922A (en) * | 1988-12-09 | 1990-08-21 | Hughes Aircraft Company | Satellite control system |
| US5025381A (en) * | 1990-01-02 | 1991-06-18 | General Electric Company | Attitude control compensator for flexible spacecraft |
| US5608634A (en) * | 1992-06-12 | 1997-03-04 | Martin Marietta Corp. | Low noise spacecraft body rate sensing arrangement for attitude control |
| SE9400579L (sv) * | 1994-02-21 | 1995-08-22 | Asea Brown Boveri | Förfarande för att styra en industrirobots rörelse i och i närheten av singulariteter |
| GB9403644D0 (en) * | 1994-02-25 | 1994-04-13 | Advanced Robotics Res | Manipulator controller |
| US5681012A (en) * | 1995-01-05 | 1997-10-28 | Hughes Electronics | Spacecraft control with skewed control moment gyros |
| US5667171A (en) * | 1995-04-28 | 1997-09-16 | Hughes Aircraft Company | Satellite spin axis stabilization using a single degree of freedom transverse momentum storage device |
| US5765780A (en) * | 1995-12-22 | 1998-06-16 | Hughes Electronics Corporation | Systematic vectored thrust calibration method for satellite momentum control |
| US5806804A (en) * | 1996-11-12 | 1998-09-15 | Lockheed Martin Corp. | Adaptive harmonic disturbance compensation system |
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1998
- 1998-03-16 US US09/042,515 patent/US6128556A/en not_active Expired - Fee Related
-
1999
- 1999-03-15 JP JP2000536623A patent/JP4249901B2/ja not_active Expired - Fee Related
- 1999-03-15 DE DE69927005T patent/DE69927005T2/de not_active Expired - Lifetime
- 1999-03-15 EP EP99912570A patent/EP1064197B1/en not_active Expired - Lifetime
- 1999-03-15 WO PCT/US1999/005703 patent/WO1999047420A1/en active IP Right Grant