AU1324001A - Momentum position control - Google Patents
Momentum position controlInfo
- Publication number
- AU1324001A AU1324001A AU13240/01A AU1324001A AU1324001A AU 1324001 A AU1324001 A AU 1324001A AU 13240/01 A AU13240/01 A AU 13240/01A AU 1324001 A AU1324001 A AU 1324001A AU 1324001 A AU1324001 A AU 1324001A
- Authority
- AU
- Australia
- Prior art keywords
- position control
- motions
- momentum
- momentum position
- combination
- 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.)
- Abandoned
Links
- 230000033001 locomotion Effects 0.000 abstract 2
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
-
- 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
- B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
-
- 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
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Chemical & Material Sciences (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Vehicle Body Suspensions (AREA)
- Navigation (AREA)
- Control Of Position Or Direction (AREA)
- Operation Control Of Excavators (AREA)
- Paper (AREA)
- Body Structure For Vehicles (AREA)
- Air Bags (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09340806 | 1999-06-28 | ||
| 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 (1)
| Publication Number | Publication Date |
|---|---|
| AU1324001A true AU1324001A (en) | 2001-01-22 |
Family
ID=23335015
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU13240/01A Abandoned AU1324001A (en) | 1999-06-28 | 2000-06-28 | Momentum position control |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US6241194B1 (enExample) |
| EP (1) | EP1188098B1 (enExample) |
| JP (1) | JP4354144B2 (enExample) |
| AT (1) | ATE259078T1 (enExample) |
| AU (1) | AU1324001A (enExample) |
| CA (1) | CA2378157A1 (enExample) |
| DE (1) | DE60008103T2 (enExample) |
| WO (1) | WO2001002921A2 (enExample) |
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 |
| US9745082B2 (en) | 2015-06-02 | 2017-08-29 | 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 |
| US10877158B2 (en) * | 2016-12-22 | 2020-12-29 | 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 WO PCT/US2000/017717 patent/WO2001002921A2/en not_active Ceased
- 2000-06-28 DE DE60008103T patent/DE60008103T2/de not_active Expired - Lifetime
- 2000-06-28 CA CA002378157A patent/CA2378157A1/en not_active Abandoned
- 2000-06-28 AU AU13240/01A patent/AU1324001A/en not_active Abandoned
- 2000-06-28 AT AT00975149T patent/ATE259078T1/de not_active IP Right Cessation
- 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
Also Published As
| Publication number | Publication date |
|---|---|
| ATE259078T1 (de) | 2004-02-15 |
| DE60008103T2 (de) | 2004-12-09 |
| WO2001002921A3 (en) | 2001-07-26 |
| EP1188098B1 (en) | 2004-02-04 |
| US6241194B1 (en) | 2001-06-05 |
| JP2004538439A (ja) | 2004-12-24 |
| DE60008103D1 (de) | 2004-03-11 |
| EP1188098A2 (en) | 2002-03-20 |
| JP4354144B2 (ja) | 2009-10-28 |
| WO2001002921A2 (en) | 2001-01-11 |
| CA2378157A1 (en) | 2001-01-11 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MK6 | Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase |