JP2004538439A5 - - Google Patents
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- Publication number
- JP2004538439A5 JP2004538439A5 JP2001508660A JP2001508660A JP2004538439A5 JP 2004538439 A5 JP2004538439 A5 JP 2004538439A5 JP 2001508660 A JP2001508660 A JP 2001508660A JP 2001508660 A JP2001508660 A JP 2001508660A JP 2004538439 A5 JP2004538439 A5 JP 2004538439A5
- Authority
- JP
- Japan
- Prior art keywords
- control moment
- wedge
- momentum
- pair
- vehicle
- 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
Links
- 238000004642 transportation engineering Methods 0.000 description 4
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Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/340,806 US6241194B1 (en) | 1999-06-28 | 1999-06-28 | Momentum position control |
PCT/US2000/017717 WO2001002921A2 (en) | 1999-06-28 | 2000-06-28 | Momentum position control |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2004538439A JP2004538439A (ja) | 2004-12-24 |
JP2004538439A5 true JP2004538439A5 (US06633600-20031014-M00021.png) | 2007-05-10 |
JP4354144B2 JP4354144B2 (ja) | 2009-10-28 |
Family
ID=23335015
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2001508660A Expired - Fee Related JP4354144B2 (ja) | 1999-06-28 | 2000-06-28 | 輸送手段用制御システム |
Country Status (8)
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2796172B1 (fr) * | 1999-07-08 | 2001-09-21 | Cit Alcatel | Systeme pour le controle d'un satellite en attitude et procede corespondant |
US6354163B1 (en) * | 2000-05-17 | 2002-03-12 | Honeywell International Inc. | Mitigating gimbal induced disturbances in CMG arrays |
US6515221B1 (en) * | 2000-08-01 | 2003-02-04 | Honeywell International Inc. | Modular reaction wheel assembly to shield electronics on a satellite |
FR2846107B1 (fr) * | 2002-10-21 | 2005-06-24 | Cit Alcatel | Dispositif de controle d'attitude d'un satellite geostationnaire |
FR2861690B1 (fr) * | 2003-11-04 | 2006-04-07 | Eads Astrium Sas | Controle d'attitude de satellites en particulier agiles a nombre reduit de gyrodynes |
US7014150B2 (en) * | 2004-07-30 | 2006-03-21 | Honeywell International Inc. | Method and system for optimizing torque in a CMG array |
US7627404B2 (en) * | 2007-04-13 | 2009-12-01 | The Boeing Company | Singularity escape and avoidance using a virtual array rotation |
US8620496B2 (en) * | 2008-07-23 | 2013-12-31 | The Boeing Company | Systems and method of controlling a spacecraft using attitude sensors |
US8209070B2 (en) * | 2008-12-17 | 2012-06-26 | Honeywell International Inc. | Methods and systems for efficiently orienting an agile vehicle using a gyroscope array |
US8561944B2 (en) | 2010-06-17 | 2013-10-22 | Lockheed Martin Corporation | System and method for desaturation of a control moment gyroscope |
US20120160965A1 (en) * | 2010-12-23 | 2012-06-28 | Muller Ronald M | Method to achieve a rapid and low power slew of a satellite |
WO2016195852A1 (en) * | 2015-06-02 | 2016-12-08 | The Charles Stark Draper Laboratory, Inc. | Rapid slew and settle systems for small satellites |
US9551994B2 (en) | 2015-06-15 | 2017-01-24 | The Boeing Company | System and method for vehicle attitude control |
WO2018112502A1 (en) * | 2016-12-22 | 2018-06-28 | Myriota Pty Ltd | System and method for generating extended satellite ephemeris data |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3741500A (en) * | 1971-04-21 | 1973-06-26 | Sperry Rand Corp | A cmg fine attitude control system |
DE4129628A1 (de) * | 1991-09-06 | 1993-03-18 | Deutsche Aerospace | Verfahren und vorrichtung zur lageregelung eines dreiachsenstabilisierten, drallbehafteten raumfahrzeuges |
US5681012A (en) * | 1995-01-05 | 1997-10-28 | Hughes Electronics | Spacecraft control with skewed control moment gyros |
DE19510371C1 (de) * | 1995-03-22 | 1996-10-31 | Daimler Benz Aerospace Ag | Verfahren zur Sonnensuche für einen dreiachsenstabilisierten Satelliten und dreiachsenstabilisierter Satellit |
JP2937123B2 (ja) * | 1995-06-15 | 1999-08-23 | 日本電気株式会社 | 宇宙航行体及び宇宙航行体の姿勢制御方法 |
JPH09226696A (ja) * | 1996-02-22 | 1997-09-02 | Toshiba Corp | 人工衛星姿勢制御装置 |
US6053445A (en) * | 1996-09-09 | 2000-04-25 | C-1 Design Group | Fly fishing reel with isolated conical drag |
US6062512A (en) * | 1997-08-27 | 2000-05-16 | Hughes Electronics Corporation | Wobble and nutation control, and spin stabilization for a spacecraft using momentum conserving devices |
US6047927A (en) * | 1998-03-16 | 2000-04-11 | Honeywell Inc. | Escaping singularities in a satellite attitude control |
-
1999
- 1999-06-28 US US09/340,806 patent/US6241194B1/en not_active Expired - Lifetime
-
2000
- 2000-06-28 CA CA002378157A patent/CA2378157A1/en not_active Abandoned
- 2000-06-28 WO PCT/US2000/017717 patent/WO2001002921A2/en active IP Right Grant
- 2000-06-28 AU AU13240/01A patent/AU1324001A/en not_active Abandoned
- 2000-06-28 EP EP00975149A patent/EP1188098B1/en not_active Expired - Lifetime
- 2000-06-28 JP JP2001508660A patent/JP4354144B2/ja not_active Expired - Fee Related
- 2000-06-28 DE DE60008103T patent/DE60008103T2/de not_active Expired - Lifetime
- 2000-06-28 AT AT00975149T patent/ATE259078T1/de not_active IP Right Cessation
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