FR2737997B1 - Procede de commande d'orientation d'un engin spatial - Google Patents
Procede de commande d'orientation d'un engin spatialInfo
- Publication number
- FR2737997B1 FR2737997B1 FR9610297A FR9610297A FR2737997B1 FR 2737997 B1 FR2737997 B1 FR 2737997B1 FR 9610297 A FR9610297 A FR 9610297A FR 9610297 A FR9610297 A FR 9610297A FR 2737997 B1 FR2737997 B1 FR 2737997B1
- Authority
- FR
- France
- Prior art keywords
- orientation
- controlling
- space machine
- space
- machine
- 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
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
-
- 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
- B64G1/36—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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (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 |
---|---|---|---|
US08/519,442 US5646847A (en) | 1995-08-25 | 1995-08-25 | Universal thruster selection logic for spacecraft attitude control |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2737997A1 FR2737997A1 (fr) | 1997-02-28 |
FR2737997B1 true FR2737997B1 (fr) | 1998-01-09 |
Family
ID=24068327
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9610297A Expired - Fee Related FR2737997B1 (fr) | 1995-08-25 | 1996-08-20 | Procede de commande d'orientation d'un engin spatial |
Country Status (2)
Country | Link |
---|---|
US (1) | US5646847A (fr) |
FR (1) | FR2737997B1 (fr) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5984237A (en) * | 1997-02-13 | 1999-11-16 | Lockheed Martin Corp. | Delta-V targeting system for three-axis controlled spacecraft |
DE19718922C1 (de) * | 1997-04-25 | 1998-04-02 | Daimler Benz Ag | Verfahren zur treibstoffminimalen, rechnergestützten Ansteuerung für beliebig an einem Raumfahrzeug angeordnete Düsen |
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 |
US8016240B2 (en) * | 2007-03-29 | 2011-09-13 | The Boeing Company | Satellites and satellite fleet implementation methods and apparatus |
US8306674B2 (en) * | 2009-10-01 | 2012-11-06 | Raytheon Company | System and method for divert and attitude control in flight vehicles |
US9638554B2 (en) | 2012-05-08 | 2017-05-02 | Nuclear Engineering, Ltd. | Strain gauge holder |
US9334068B2 (en) * | 2014-04-04 | 2016-05-10 | NOA Inc. | Unified orbit and attitude control for nanosatellites using pulsed ablative thrusters |
US10005568B2 (en) | 2015-11-13 | 2018-06-26 | The Boeing Company | Energy efficient satellite maneuvering |
US10220966B2 (en) | 2016-04-05 | 2019-03-05 | Raytheon Company | Satellite with integral thrusters |
CN108639384A (zh) * | 2018-04-03 | 2018-10-12 | 上海航天控制技术研究所 | 一种基于姿控推力器复用的卫星推进剂管理方法 |
US11718422B2 (en) | 2020-09-30 | 2023-08-08 | Maxar Space Llc | Systems and methods for satellite movement |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3866025A (en) * | 1972-03-17 | 1975-02-11 | Rca Corp | Spacecraft attitude control system |
US4599697A (en) * | 1982-08-11 | 1986-07-08 | Ford Aerospace & Communications Corporation | Digital PWPF three axis spacecraft attitude control |
US4537375A (en) * | 1983-04-21 | 1985-08-27 | Ford Aerospace & Communications Corporation | Method and apparatus for thruster transient control |
JP2518212B2 (ja) * | 1986-06-26 | 1996-07-24 | 日本電気株式会社 | 人工衛星の軌道制御方式 |
US4848706A (en) * | 1988-02-29 | 1989-07-18 | Ford Aerospace Corporation | Spacecraft attitude control using coupled thrusters |
US4961551A (en) * | 1988-11-18 | 1990-10-09 | Hughes Aircraft Company | Stabilization of a spinning spacecraft of arbitary shape |
US5098041A (en) * | 1990-06-07 | 1992-03-24 | Hughes Aircraft Company | Attitude control system for momentum-biased spacecraft |
US5130931A (en) * | 1990-07-13 | 1992-07-14 | General Electric Company | Spacecraft attitude and velocity control system |
US5140525A (en) * | 1991-07-31 | 1992-08-18 | General Electric Company | Unified spacecraft attitude control system |
CA2076894C (fr) * | 1991-11-27 | 1998-11-03 | John F. Yocum | Modulation de poussee tri-axiale |
US5400252A (en) * | 1992-12-22 | 1995-03-21 | Space Systems/Loral, Inc. | Spacecraft East/West orbit control during a North or South stationkeeping maneuver |
US5335179A (en) * | 1992-12-24 | 1994-08-02 | General Electric Co. | Unified spacecraft attitude control system with pseudo-complementary paired thrusters |
-
1995
- 1995-08-25 US US08/519,442 patent/US5646847A/en not_active Expired - Lifetime
-
1996
- 1996-08-20 FR FR9610297A patent/FR2737997B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2737997A1 (fr) | 1997-02-28 |
US5646847A (en) | 1997-07-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20150430 |