IT1317682B1 - Regolazione di posizione triassiale per satelliti ad orbita bassa - Google Patents
Regolazione di posizione triassiale per satelliti ad orbita bassaInfo
- Publication number
- IT1317682B1 IT1317682B1 IT2000MI001172A ITMI20001172A IT1317682B1 IT 1317682 B1 IT1317682 B1 IT 1317682B1 IT 2000MI001172 A IT2000MI001172 A IT 2000MI001172A IT MI20001172 A ITMI20001172 A IT MI20001172A IT 1317682 B1 IT1317682 B1 IT 1317682B1
- Authority
- IT
- Italy
- Prior art keywords
- tri
- position adjustment
- axial position
- low orbit
- orbit satellites
- 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
- B64G1/36—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
-
- 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
- B64G1/244—Spacecraft control systems
- B64G1/245—Attitude control algorithms for spacecraft attitude control
-
- 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
- B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun 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
- B64G1/26—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
- B64G1/28—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
-
- 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
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)
- Environmental & Geological Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Geology (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Measuring Magnetic Variables (AREA)
- Navigation (AREA)
- Radio Relay Systems (AREA)
- Control Of Position Or Direction (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19924908A DE19924908B4 (de) | 1999-05-31 | 1999-05-31 | Verfahren zur dreiachsigen Lagebestimmung für einen niedrig fliegenden Satelliten |
Publications (3)
Publication Number | Publication Date |
---|---|
ITMI20001172A0 ITMI20001172A0 (it) | 2000-05-26 |
ITMI20001172A1 ITMI20001172A1 (it) | 2001-11-26 |
IT1317682B1 true IT1317682B1 (it) | 2003-07-15 |
Family
ID=7909772
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT2000MI001172A IT1317682B1 (it) | 1999-05-31 | 2000-05-26 | Regolazione di posizione triassiale per satelliti ad orbita bassa |
Country Status (5)
Country | Link |
---|---|
US (1) | US6685142B1 (it) |
DE (1) | DE19924908B4 (it) |
FR (1) | FR2794254B1 (it) |
GB (1) | GB2350596B (it) |
IT (1) | IT1317682B1 (it) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10226535A1 (de) * | 2002-06-14 | 2004-01-08 | Astrium Gmbh | Dreiachsige Lagebestimmung eines Satelliten durch zeitliche Propagation von zweiachsigen Sensor-Messwerten |
US7246775B1 (en) * | 2004-08-02 | 2007-07-24 | Lockheed Martin Corporation | System and method of substantially autonomous geosynchronous time-optimal orbit transfer |
US8020809B2 (en) * | 2007-04-18 | 2011-09-20 | Ithaco Space Systems, Inc. | Direct torque actuator control for control moment gyroscope |
US8686721B2 (en) | 2012-02-27 | 2014-04-01 | The Johns Hopkins University | Automated pre-processing of body-mounted magnetometer data from constellations of low earth orbit satellites for derivation of birkeland current signatures |
CN105253330B (zh) * | 2015-10-30 | 2017-04-05 | 中国空间技术研究院 | 一种基于优化的信息融合geo卫星控制系统菜单式设计方法 |
US10005568B2 (en) * | 2015-11-13 | 2018-06-26 | The Boeing Company | Energy efficient satellite maneuvering |
RU2618664C1 (ru) * | 2016-01-25 | 2017-05-05 | Акционерное общество "Научно-исследовательский институт электромеханики" (АО "НИИЭМ") | Способ ориентации космического аппарата и устройство для реализации способа |
RU2691536C1 (ru) * | 2018-02-13 | 2019-06-14 | Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" | Способ определения трехосной ориентации космического аппарата |
CN110816898B (zh) * | 2019-11-01 | 2021-04-27 | 上海卫星工程研究所 | 大角动量补偿卫星三级失稳判断与控制设计方法 |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3061239A (en) * | 1960-08-04 | 1962-10-30 | Lockheed Aircraft Corp | Magnetic moment device for applying corrective torque to a space vehicle |
US3429524A (en) * | 1965-07-19 | 1969-02-25 | Westinghouse Electric Corp | Attitude control system |
US3489372A (en) * | 1967-07-31 | 1970-01-13 | Us Navy | Satellite spin control system |
JPS491439B1 (it) * | 1968-09-27 | 1974-01-14 | ||
JPS537720B1 (it) * | 1970-07-29 | 1978-03-20 | ||
US3834653A (en) * | 1972-03-27 | 1974-09-10 | Rca Corp | Closed loop roll and yaw control for satellites |
DE3606636C1 (de) * | 1986-02-28 | 1987-11-05 | Messerschmitt Boelkow Blohm | Verfahren zur Bestimmung von Erdmagnetfeldkomponenten bezueglich eines satellitenfesten Koordinatensystems |
US4807835A (en) * | 1987-04-10 | 1989-02-28 | Ithaco, Inc. | Spacecraft attitude stabilization system |
US4883244A (en) * | 1987-12-23 | 1989-11-28 | Hughes Aircraft Company | Satellite attitude determination and control system with agile beam sensing |
CA1321418C (en) * | 1988-10-05 | 1993-08-17 | Joseph C. Mcmillan | Primary land arctic navigation system |
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 |
US5047945A (en) * | 1990-08-09 | 1991-09-10 | General Electric Company | Residual magnetic dipole cancellation system for satellites |
CA2080612A1 (en) * | 1991-11-27 | 1993-05-28 | Douglas J. Bender | Method and apparatus for compensating for magnetic disturbance torques on a satellite |
US5354016A (en) * | 1992-07-30 | 1994-10-11 | General Electric Co. | Pivoted wheel roll control with automatic offset |
FR2717149B1 (fr) * | 1994-03-11 | 1996-05-31 | Aerospatiale | Procédé adaptatif de contrôle d'attitude pour stabiliser magnétiquement un satellite au moins en roulis-lacet. |
DE4432265C2 (de) * | 1994-09-10 | 1996-12-12 | Daimler Benz Aerospace Ag | Verfahren zur Bestimmung des Drehimpulsvektors eines Satelliten |
DE19518617A1 (de) * | 1995-05-24 | 1996-11-28 | Daimler Benz Aerospace Ag | Dreiachsenstabilisierter, erdorientierter Satellit und zugehöriges Sonnen- und Erdakquisitonsverfahren unter Benutzung eines Magnetometers |
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 |
US5826829A (en) * | 1996-07-15 | 1998-10-27 | Space Systems/Loral Inc. | Spacecraft control system with a trihedral momentum bias wheel configuration |
US6113034A (en) * | 1997-08-04 | 2000-09-05 | Motorola, Inc. | Method and apparatus for estimating effects of disturbance forces |
DE19816978C1 (de) * | 1998-04-17 | 1999-11-04 | Daimler Chrysler Ag | Verfahren zur Identifizierung eines fehlerhaft messenden Sensors in einem Raumfahrzeug |
-
1999
- 1999-05-31 DE DE19924908A patent/DE19924908B4/de not_active Expired - Fee Related
-
2000
- 2000-05-25 GB GB0012833A patent/GB2350596B/en not_active Expired - Fee Related
- 2000-05-26 IT IT2000MI001172A patent/IT1317682B1/it active
- 2000-05-30 FR FR0006891A patent/FR2794254B1/fr not_active Expired - Lifetime
- 2000-05-31 US US09/583,340 patent/US6685142B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US6685142B1 (en) | 2004-02-03 |
ITMI20001172A1 (it) | 2001-11-26 |
GB2350596B (en) | 2002-02-13 |
FR2794254B1 (fr) | 2005-01-28 |
ITMI20001172A0 (it) | 2000-05-26 |
FR2794254A1 (fr) | 2000-12-01 |
GB2350596A (en) | 2000-12-06 |
GB0012833D0 (en) | 2000-07-19 |
DE19924908A1 (de) | 2000-12-07 |
DE19924908B4 (de) | 2008-05-29 |
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