FR2693282B1 - Système et procédé pour commander l'attitude d'un engin spatial. - Google Patents
Système et procédé pour commander l'attitude d'un engin spatial.Info
- Publication number
- FR2693282B1 FR2693282B1 FR9305721A FR9305721A FR2693282B1 FR 2693282 B1 FR2693282 B1 FR 2693282B1 FR 9305721 A FR9305721 A FR 9305721A FR 9305721 A FR9305721 A FR 9305721A FR 2693282 B1 FR2693282 B1 FR 2693282B1
- Authority
- FR
- France
- Prior art keywords
- spacecraft
- attitude
- controlling
- 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.)
- Expired - Fee Related
Links
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
- B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
-
- 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
-
- 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
- B64G1/365—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth sensors
-
- 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
- B64G1/366—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using magnetometers
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Environmental & Geological Engineering (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Geology (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/882,507 US5248118A (en) | 1992-05-13 | 1992-05-13 | Spacecraft attitude control system with reaction wheel bearing protection |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2693282A1 FR2693282A1 (fr) | 1994-01-07 |
FR2693282B1 true FR2693282B1 (fr) | 1995-02-17 |
Family
ID=25380745
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9305721A Expired - Fee Related FR2693282B1 (fr) | 1992-05-13 | 1993-05-12 | Système et procédé pour commander l'attitude d'un engin spatial. |
Country Status (3)
Country | Link |
---|---|
US (1) | US5248118A (fr) |
JP (1) | JPH0624396A (fr) |
FR (1) | FR2693282B1 (fr) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5610820A (en) * | 1995-03-23 | 1997-03-11 | Martin Marietta Corp. | Minimum propellant, zero momentum spacecraft attitude control system |
US5787368A (en) * | 1995-11-03 | 1998-07-28 | Space Systems/Loral, Inc. | Spacecraft yaw control using only wheel speed measurements processed through a simple filter bank |
FR2742122B1 (fr) * | 1995-12-06 | 1998-02-06 | Matra Marconi Space France | Procede et dispositif de commande d'attitude de satellite a generateurs solaires |
FR2742243B1 (fr) * | 1995-12-06 | 1998-02-13 | Matra Marconi Space France | Procede de commande d'attitude d'un satellite en orbite basse, a acquisition solaire |
US5992799A (en) * | 1996-03-08 | 1999-11-30 | Space Systems/Loral, Inc. | Earth based spacecraft orbit and attitude control using a look-ahead thruster selection logic and magnetic torquers |
US5826829A (en) * | 1996-07-15 | 1998-10-27 | Space Systems/Loral Inc. | Spacecraft control system with a trihedral momentum bias wheel configuration |
US5996942A (en) * | 1996-10-16 | 1999-12-07 | Space Systems/Loral, Inc. | Autonomous solar torque management |
US5935176A (en) * | 1996-11-22 | 1999-08-10 | Lockheed Martin Corporation | Momentum wheel oscillation filter |
US6047927A (en) * | 1998-03-16 | 2000-04-11 | Honeywell Inc. | Escaping singularities in a satellite attitude control |
US6356814B1 (en) * | 1999-02-03 | 2002-03-12 | Microcosm, Inc. | Spacecraft magnetic torquer feedback system |
US6254036B1 (en) * | 2000-02-16 | 2001-07-03 | Hughes Electronics Corporation | Method and apparatus for spacecraft wheel desaturation |
US6550721B2 (en) * | 2000-03-09 | 2003-04-22 | The Boeing Company | Safing mode for high momentum states in body stabilized spacecraft |
US6732977B1 (en) | 2002-02-11 | 2004-05-11 | Lockheed Martin Corporation | System for on-orbit correction of spacecraft payload pointing errors |
US6695263B1 (en) | 2002-02-12 | 2004-02-24 | Lockheed Martin Corporation | System for geosynchronous spacecraft rapid earth reacquisition |
US7051980B2 (en) * | 2002-02-26 | 2006-05-30 | Lockheed Martin Corporation | Efficient orbit sparing system for space vehicle constellations |
US6702234B1 (en) | 2002-03-29 | 2004-03-09 | Lockheed Martin Corporation | Fault tolerant attitude control system for zero momentum spacecraft |
US7835826B1 (en) | 2005-12-13 | 2010-11-16 | Lockheed Martin Corporation | Attitude determination system for yaw-steering spacecraft |
US8412391B2 (en) * | 2007-08-17 | 2013-04-02 | Princeton Satelitte Systems | Proximity spacecraft maneuvering |
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 |
US8918236B2 (en) | 2011-06-24 | 2014-12-23 | Honeywell International Inc. | Methods and systems for adjusting attitude using reaction wheels |
US10005568B2 (en) * | 2015-11-13 | 2018-06-26 | The Boeing Company | Energy efficient satellite maneuvering |
US10752385B2 (en) * | 2017-03-09 | 2020-08-25 | Princeton Satellite Systems, Inc. | Magnetic dipole cancellation |
CN111056045B (zh) * | 2019-12-26 | 2021-03-23 | 航天行云科技有限公司 | 一种三轴磁力矩器的控制方法以及装置 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4010921A (en) * | 1975-08-20 | 1977-03-08 | The United States Of America As Represented By The Secretary Of The Air Force | Spacecraft closed loop three-axis momentum unloading system |
FR2655167B1 (fr) * | 1989-11-29 | 1992-04-03 | Aerospatiale | Procede de controle d'attitude en roulis et en lacet d'un satellite. |
US5020745A (en) * | 1989-12-20 | 1991-06-04 | General Electric Company | Reaction wheel fricton compensation using dither |
US5123617A (en) * | 1990-03-05 | 1992-06-23 | General Electric Company | Spacecraft momentum unloading using controlled magnetic torques |
US5058835A (en) * | 1990-06-11 | 1991-10-22 | General Electric Company | Wheel speed management control system for spacecraft |
US5201833A (en) * | 1991-07-19 | 1993-04-13 | General Electric Company | Attitude control system with reaction wheel friction compensation |
-
1992
- 1992-05-13 US US07/882,507 patent/US5248118A/en not_active Expired - Lifetime
-
1993
- 1993-05-11 JP JP5108637A patent/JPH0624396A/ja not_active Withdrawn
- 1993-05-12 FR FR9305721A patent/FR2693282B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US5248118A (en) | 1993-09-28 |
FR2693282A1 (fr) | 1994-01-07 |
JPH0624396A (ja) | 1994-02-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property | ||
ST | Notification of lapse |
Effective date: 20060131 |