FR2581966B1 - Procede et systeme de stabilisation d'un vehicule spatial - Google Patents
Procede et systeme de stabilisation d'un vehicule spatialInfo
- Publication number
- FR2581966B1 FR2581966B1 FR868607094A FR8607094A FR2581966B1 FR 2581966 B1 FR2581966 B1 FR 2581966B1 FR 868607094 A FR868607094 A FR 868607094A FR 8607094 A FR8607094 A FR 8607094A FR 2581966 B1 FR2581966 B1 FR 2581966B1
- Authority
- FR
- France
- Prior art keywords
- stabilizing
- space vehicle
- vehicle
- space
- 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
- 230000000087 stabilizing effect Effects 0.000 title 1
Classifications
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/52—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of an outer space vehicle
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/14—Space shuttles
-
- 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
- B64G1/281—Spin-stabilised spacecraft
-
- 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
- B64G1/38—Guiding or controlling apparatus, e.g. for attitude control damping of oscillations, e.g. nutation dampers
-
- 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
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
- B64G1/369—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using gyroscopes as attitude sensors
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- Theoretical Computer Science (AREA)
- Educational Technology (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Educational Administration (AREA)
- Physics & Mathematics (AREA)
- Business, Economics & Management (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Navigation (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/735,260 US4758957A (en) | 1985-05-17 | 1985-05-17 | Spacecraft stabilization system and method |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2581966A1 FR2581966A1 (fr) | 1986-11-21 |
FR2581966B1 true FR2581966B1 (fr) | 1990-02-02 |
Family
ID=24955020
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR868607094A Expired - Fee Related FR2581966B1 (fr) | 1985-05-17 | 1986-05-16 | Procede et systeme de stabilisation d'un vehicule spatial |
Country Status (2)
Country | Link |
---|---|
US (1) | US4758957A (fr) |
FR (1) | FR2581966B1 (fr) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
DE3885883D1 (de) * | 1987-09-16 | 1994-01-05 | Deutsche Aerospace | Vorrichtung zur sollwertregelung und/oder stabilisierung von freibeweglichen körpern mit gespeichertem drall. |
FR2630398B1 (fr) * | 1988-04-26 | 1990-08-24 | Aerospatiale | Procede de basculement du moment d'inertie d'un corps rotatif libre dans l'espace jusqu'en une direction donnee |
US4931942A (en) * | 1988-05-26 | 1990-06-05 | Ford Aerospace Corporation | Transition control system for spacecraft attitude control |
US5092543A (en) * | 1989-09-27 | 1992-03-03 | General Electric Company | Spacecraft attitude control with avoidance constraint |
US5124925A (en) * | 1990-01-16 | 1992-06-23 | Space Systems/Loral, Inc. | Method for controlling east/west motion of a geostationary satellite |
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 |
US5163640A (en) * | 1990-12-14 | 1992-11-17 | Hughes Aircraft Company | Active spin axis control for spinning space vehicles |
US5222023A (en) * | 1991-04-02 | 1993-06-22 | Space Systems/Loral, Inc. | Compensated transition for spacecraft attitude control |
US5267167A (en) * | 1991-05-10 | 1993-11-30 | Ball Corporation | Method and system for formationfinding and formationkeeping in a constellation of satellites |
US5140525A (en) * | 1991-07-31 | 1992-08-18 | General Electric Company | Unified spacecraft attitude control system |
US5608634A (en) * | 1992-06-12 | 1997-03-04 | Martin Marietta Corp. | Low noise spacecraft body rate sensing arrangement for attitude control |
US5308025A (en) * | 1992-07-30 | 1994-05-03 | Hughes Aircraft Company | Spacecraft spin axis capture system and method |
US5456429A (en) * | 1993-08-02 | 1995-10-10 | Loral Corp. | Thrust maneuver system |
US5459669A (en) * | 1994-02-14 | 1995-10-17 | Space Systems/Loral, Inc. | Control system and method for spacecraft attitude control |
US5884869A (en) * | 1996-03-18 | 1999-03-23 | Hughes Electronics Corporation | Satellite spin vector control with sun sensor |
JP3034807B2 (ja) * | 1996-08-30 | 2000-04-17 | 三菱電機株式会社 | 人工衛星の姿勢決定装置 |
US6068217A (en) * | 1996-10-16 | 2000-05-30 | Space Systems/Loral, Inc. | Method to reorient a spacecraft using only initial single axis attitude knowledge |
US6000661A (en) * | 1996-10-16 | 1999-12-14 | Space Systems/Loral, Inc. | Autonomous spacecraft payload base motion estimation and correction |
US5996942A (en) * | 1996-10-16 | 1999-12-07 | Space Systems/Loral, Inc. | Autonomous solar torque management |
US6023291A (en) * | 1996-10-16 | 2000-02-08 | Space Systems/Loral, Inc. | Satellite camera attitude determination and image navigation by means of earth edge and landmark measurement |
US6125310A (en) * | 1997-07-18 | 2000-09-26 | Space Systems/Loral, Inc. | Thruster on time signaling with flexure compensation avoidance |
US6496741B1 (en) | 1999-03-25 | 2002-12-17 | Gregory J. Whiffen | Static/dynamic control for optimizing a useful objective |
US6347262B1 (en) * | 2000-01-05 | 2002-02-12 | Hughes Electronics Corporation | Minimum fuel attitude and nutation controller for spinning spacecraft |
GB0125728D0 (en) * | 2001-10-26 | 2001-12-19 | Astrium Ltd | Autonomous active manoeuvring method and system for spinning spacecraft |
US7437222B2 (en) * | 2005-07-28 | 2008-10-14 | The Boeing Company | Gimbal disturbance calibration and compenstion |
US8019493B1 (en) * | 2007-07-20 | 2011-09-13 | Lockheed Martin Corporation | Spacecraft thruster torque feedforward calibration system |
RU2657809C1 (ru) * | 2017-03-30 | 2018-06-15 | Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" | Способ определения угловой скорости собственного вращения космического аппарата вокруг центра масс |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS491439B1 (fr) * | 1968-09-27 | 1974-01-14 | ||
JPS537720B1 (fr) * | 1970-07-29 | 1978-03-20 | ||
US3705977A (en) * | 1970-10-14 | 1972-12-12 | Gen Electric | Attitude control system |
US3866025A (en) * | 1972-03-17 | 1975-02-11 | Rca Corp | Spacecraft attitude control system |
US3944172A (en) * | 1972-04-14 | 1976-03-16 | Erno Raumfahrttechnik Gmbh | Attitude control for space vehicle |
US3940096A (en) * | 1974-11-27 | 1976-02-24 | Rca Corporation | Re-orientation of a spacecraft relative to its angular momentum vector |
US4071211A (en) * | 1976-09-23 | 1978-01-31 | Rca Corporation | Momentum biased active three-axis satellite attitude control system |
FR2369612A1 (fr) * | 1976-10-27 | 1978-05-26 | Matra | Perfectionnements aux dispositifs de commande d'attitude pour vehicules |
FR2373823A1 (fr) * | 1976-12-10 | 1978-07-07 | Matra | Procede et dispositif de commande d'attitude de vehicule spatial |
FR2447320A1 (fr) * | 1979-01-23 | 1980-08-22 | Matra | Perfectionnements aux procedes et dispositifs d'amortissement actif de nutation pour vehicule spatial |
US4306692A (en) * | 1979-03-16 | 1981-12-22 | Communications Satellite Corporation | Attitude acquisition maneuver for a bias momentum spacecraft |
US4471926A (en) * | 1979-10-29 | 1984-09-18 | Trw Inc. | Transfer vehicle for use in conjunction with a reusable space shuttle |
US4386750A (en) * | 1980-08-29 | 1983-06-07 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method of damping nutation motion with minimum spin axis attitude disturbance |
US4599697A (en) * | 1982-08-11 | 1986-07-08 | Ford Aerospace & Communications Corporation | Digital PWPF three axis spacecraft attitude control |
-
1985
- 1985-05-17 US US06/735,260 patent/US4758957A/en not_active Expired - Lifetime
-
1986
- 1986-05-16 FR FR868607094A patent/FR2581966B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2581966A1 (fr) | 1986-11-21 |
US4758957A (en) | 1988-07-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |