ATE458216T1 - Vorrichtung zur lagesteuerung eines geostationären satelliten - Google Patents
Vorrichtung zur lagesteuerung eines geostationären satellitenInfo
- Publication number
- ATE458216T1 ATE458216T1 AT03292442T AT03292442T ATE458216T1 AT E458216 T1 ATE458216 T1 AT E458216T1 AT 03292442 T AT03292442 T AT 03292442T AT 03292442 T AT03292442 T AT 03292442T AT E458216 T1 ATE458216 T1 AT E458216T1
- Authority
- AT
- Austria
- Prior art keywords
- geostationary satellite
- position control
- satellite
- structures
- attitude
- Prior art date
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
- B64G1/244—Spacecraft control systems
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Automation & Control Theory (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Radio Relay Systems (AREA)
- Selective Calling Equipment (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0213052A FR2846107B1 (fr) | 2002-10-21 | 2002-10-21 | Dispositif de controle d'attitude d'un satellite geostationnaire |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE458216T1 true ATE458216T1 (de) | 2010-03-15 |
Family
ID=32050561
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT03292442T ATE458216T1 (de) | 2002-10-21 | 2003-10-03 | Vorrichtung zur lagesteuerung eines geostationären satelliten |
Country Status (6)
Country | Link |
---|---|
US (1) | US20040122568A1 (de) |
EP (1) | EP1413940B1 (de) |
AT (1) | ATE458216T1 (de) |
DE (1) | DE60331280D1 (de) |
ES (1) | ES2338644T3 (de) |
FR (1) | FR2846107B1 (de) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110005316A1 (en) * | 2005-07-12 | 2011-01-13 | Centro De Investigacon De Rotagcion Y Torque S.L | Acceleration systems for moving devices |
US10484095B2 (en) * | 2017-06-15 | 2019-11-19 | The Aerospace Corporation | Communications relay satellite with a single-axis gimbal |
CN109164817B (zh) * | 2018-07-27 | 2021-09-14 | 西北工业大学 | 一种基于模型预测控制的太阳帆姿态轨道耦合控制方法 |
FR3094479B1 (fr) * | 2019-03-25 | 2021-08-27 | Airbus Defence & Space Sas | Dispositif et procédé de détermination d’attitude d’un satellite équipé d’actionneurs gyroscopiques, et satellite embarquant un tel dispositif |
WO2021232032A2 (en) | 2020-02-13 | 2021-11-18 | Ast & Science, Llc | System for tracking solar energy |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3071249D1 (en) * | 1980-08-19 | 1986-01-02 | Messerschmitt Boelkow Blohm | Attitude control device for elastic vehicles |
FR2647565B1 (fr) * | 1989-04-24 | 1991-07-26 | Alcatel Espace | Procede de mise a poste d'un satellite de telecommunications geostationnaire |
US6089507A (en) * | 1996-12-05 | 2000-07-18 | Parvez; Shabbir Ahmed | Autonomous orbit control with position and velocity feedback using modern control theory |
US5944761A (en) * | 1997-06-06 | 1999-08-31 | Honeywell Inc. | Variable periodic disturbance rejection filter |
US5931419A (en) * | 1997-08-07 | 1999-08-03 | Honeywell Inc. | Reducing satellite weight and cost |
US6267876B1 (en) * | 1998-07-31 | 2001-07-31 | Trinity Flywheel Power | Control of magnetic bearing-supported rotors |
US6152403A (en) * | 1998-11-11 | 2000-11-28 | Hughes Electronics Corporation | Gyroscopic calibration methods for spacecraft |
US6241194B1 (en) * | 1999-06-28 | 2001-06-05 | Honeywell International Inc. | Momentum position control |
FR2796172B1 (fr) * | 1999-07-08 | 2001-09-21 | Cit Alcatel | Systeme pour le controle d'un satellite en attitude et procede corespondant |
FR2819597B1 (fr) * | 2001-01-15 | 2003-04-11 | Cit Alcatel | Procede de guidage d'un systeme d'actionneurs gyrospcopiques |
US6607167B2 (en) * | 2001-02-01 | 2003-08-19 | The Boeing Company | Spacecraft thermal shock suppression system |
FR2826470B1 (fr) * | 2001-06-26 | 2003-09-19 | Astrium Sas | Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes |
US6891498B2 (en) * | 2002-03-28 | 2005-05-10 | Honeywell International Inc. | Inertial reference system for a spacecraft |
WO2004032392A2 (en) * | 2002-08-28 | 2004-04-15 | Arizona Board Of Regents | Steering logic for control moment gyro system |
JP3970724B2 (ja) * | 2002-08-30 | 2007-09-05 | Nec東芝スペースシステム株式会社 | 飛翔体の姿勢変更制御装置及び姿勢変更制御方法 |
-
2002
- 2002-10-21 FR FR0213052A patent/FR2846107B1/fr not_active Expired - Fee Related
-
2003
- 2003-10-03 ES ES03292442T patent/ES2338644T3/es not_active Expired - Lifetime
- 2003-10-03 AT AT03292442T patent/ATE458216T1/de not_active IP Right Cessation
- 2003-10-03 DE DE60331280T patent/DE60331280D1/de not_active Expired - Lifetime
- 2003-10-03 EP EP03292442A patent/EP1413940B1/de not_active Expired - Lifetime
- 2003-10-20 US US10/687,585 patent/US20040122568A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
EP1413940B1 (de) | 2010-02-17 |
FR2846107A1 (fr) | 2004-04-23 |
ES2338644T3 (es) | 2010-05-11 |
FR2846107B1 (fr) | 2005-06-24 |
DE60331280D1 (de) | 2010-04-01 |
US20040122568A1 (en) | 2004-06-24 |
EP1413940A1 (de) | 2004-04-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |