FR2525359B1 - Procede et dispositif de regulation d'attitude d'un satellite terrestre artificiel - Google Patents
Procede et dispositif de regulation d'attitude d'un satellite terrestre artificielInfo
- Publication number
- FR2525359B1 FR2525359B1 FR838306423A FR8306423A FR2525359B1 FR 2525359 B1 FR2525359 B1 FR 2525359B1 FR 838306423 A FR838306423 A FR 838306423A FR 8306423 A FR8306423 A FR 8306423A FR 2525359 B1 FR2525359 B1 FR 2525359B1
- Authority
- FR
- France
- Prior art keywords
- attitude
- regulating
- terrestrial satellite
- artificial terrestrial
- artificial
- 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 - Lifetime
Links
- 230000001105 regulatory effect Effects 0.000 title 1
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
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/285—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum wheels
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)
- Life Sciences & Earth Sciences (AREA)
- Environmental & Geological Engineering (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Geology (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19823214373 DE3214373A1 (de) | 1982-04-20 | 1982-04-20 | Verfahren und einrichtung fuer die lageregelung eines satelliten |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2525359A1 FR2525359A1 (fr) | 1983-10-21 |
FR2525359B1 true FR2525359B1 (fr) | 1990-03-30 |
Family
ID=6161257
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR838306423A Expired - Lifetime FR2525359B1 (fr) | 1982-04-20 | 1983-04-20 | Procede et dispositif de regulation d'attitude d'un satellite terrestre artificiel |
Country Status (4)
Country | Link |
---|---|
JP (1) | JPS58183395A (it) |
DE (1) | DE3214373A1 (it) |
FR (1) | FR2525359B1 (it) |
GB (1) | GB2121984B (it) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3606636C1 (de) * | 1986-02-28 | 1987-11-05 | Messerschmitt Boelkow Blohm | Verfahren zur Bestimmung von Erdmagnetfeldkomponenten bezueglich eines satellitenfesten Koordinatensystems |
US4916622A (en) * | 1988-06-16 | 1990-04-10 | General Electric Company | Attitude control system |
GB2241480B (en) * | 1990-02-28 | 1993-05-26 | British Aerospace | Apparatus and method for controlling attitude of a spacecraft orbiting earth or other celestial body |
DE4007497A1 (de) * | 1990-03-09 | 1991-09-12 | Messerschmitt Boelkow Blohm | Vorrichtung zur lageregelung von raumstationen |
FR2670745B1 (fr) * | 1990-12-21 | 1993-04-16 | Aerospatiale | Systeme de controle d'attitude pour satellite stabilise 3-axes sur orbite a faible inclinaison. |
FR2678894B1 (fr) * | 1991-07-09 | 1993-11-19 | Aerospatiale Ste Nationale Indle | Procede et dispositif de controle d'attitude en roulis-lacet d'un satellite a direction unique d'actionnement continu. |
CA2080612A1 (en) * | 1991-11-27 | 1993-05-28 | Douglas J. Bender | Method and apparatus for compensating for magnetic disturbance torques on a satellite |
FR2718105B1 (fr) * | 1994-03-30 | 1996-06-14 | Centre Nat Etd Spatiales | Satellite artificiel muni de générateurs de moments magnétiques et aérodynamiques et procédé de commande d'un tel satellite. |
FR2724364B1 (fr) * | 1994-09-12 | 1997-01-17 | Matra Marconi Space France | Procede et systeme de stabilisation selon trois axes d'un satellite d'orbite non-equatoriale |
DE19520115A1 (de) * | 1995-06-01 | 1996-12-05 | Contraves Gmbh | Verfahren zum Bestimmen der Rollage eines rollenden Flugobjektes |
JP5595978B2 (ja) * | 2011-05-28 | 2014-09-24 | 双葉電子工業株式会社 | 遠隔制御機器の駆動制御装置 |
CN108021138B (zh) * | 2017-11-03 | 2020-05-19 | 西北工业大学 | 一种地磁场模型简化设计方法 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3189298A (en) * | 1962-08-06 | 1965-06-15 | Westinghouse Electric Corp | Control apparatus for spacecraft |
US3834653A (en) * | 1972-03-27 | 1974-09-10 | Rca Corp | Closed loop roll and yaw control for satellites |
CA1073988A (en) * | 1975-07-21 | 1980-03-18 | Ludwig Muhlfelder | Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbits |
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 |
JPS5628100A (en) * | 1979-08-15 | 1981-03-19 | Mitsubishi Electric Corp | Wheel unloading device |
JPS56131500A (en) * | 1980-03-21 | 1981-10-15 | Mitsubishi Electric Corp | Magnetic controlling system for triaxes controlling satellite |
US4521855A (en) * | 1981-07-27 | 1985-06-04 | Ford Aerospace & Communications Corporation | Electronic on-orbit roll/yaw satellite control |
-
1982
- 1982-04-20 DE DE19823214373 patent/DE3214373A1/de active Granted
-
1983
- 1983-03-31 JP JP58056773A patent/JPS58183395A/ja active Granted
- 1983-04-14 GB GB08310161A patent/GB2121984B/en not_active Expired
- 1983-04-20 FR FR838306423A patent/FR2525359B1/fr not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE3214373A1 (de) | 1983-10-27 |
DE3214373C2 (it) | 1987-10-15 |
GB2121984B (en) | 1986-01-29 |
JPS58183395A (ja) | 1983-10-26 |
GB2121984A (en) | 1984-01-04 |
FR2525359A1 (fr) | 1983-10-21 |
JPH0468199B2 (it) | 1992-10-30 |
GB8310161D0 (en) | 1983-05-18 |
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