FR2661261A1 - Commande d'attitude tridimensionnelle d'un engin spatial utilisant un detecteur d'etoile polaire. - Google Patents
Commande d'attitude tridimensionnelle d'un engin spatial utilisant un detecteur d'etoile polaire. Download PDFInfo
- Publication number
- FR2661261A1 FR2661261A1 FR9104157A FR9104157A FR2661261A1 FR 2661261 A1 FR2661261 A1 FR 2661261A1 FR 9104157 A FR9104157 A FR 9104157A FR 9104157 A FR9104157 A FR 9104157A FR 2661261 A1 FR2661261 A1 FR 2661261A1
- Authority
- FR
- France
- Prior art keywords
- signals
- spacecraft
- pitch
- roll
- star
- 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.)
- Granted
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/02—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by astronomical means
-
- 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
- B64G1/361—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using star 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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/24—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 specially adapted for cosmonautical navigation
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
- G01S3/78—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
- G01S3/782—Systems for determining direction or deviation from predetermined direction
- G01S3/785—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system
- G01S3/786—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system the desired condition being maintained automatically
- G01S3/7867—Star trackers
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- General Physics & Mathematics (AREA)
- Geology (AREA)
- Geochemistry & Mineralogy (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Environmental & Geological Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Navigation (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/511,169 US5107434A (en) | 1990-04-19 | 1990-04-19 | Three-axis spacecraft attitude control using polar star sensor |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2661261A1 true FR2661261A1 (fr) | 1991-10-25 |
FR2661261B1 FR2661261B1 (US06826419-20041130-M00005.png) | 1995-01-20 |
Family
ID=24033738
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9104157A Granted FR2661261A1 (fr) | 1990-04-19 | 1991-04-05 | Commande d'attitude tridimensionnelle d'un engin spatial utilisant un detecteur d'etoile polaire. |
Country Status (4)
Country | Link |
---|---|
US (1) | US5107434A (US06826419-20041130-M00005.png) |
JP (1) | JPH04228400A (US06826419-20041130-M00005.png) |
DE (1) | DE4112361A1 (US06826419-20041130-M00005.png) |
FR (1) | FR2661261A1 (US06826419-20041130-M00005.png) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2050674A1 (fr) * | 2007-10-19 | 2009-04-22 | Thales | Système de visée absolue améliorée par combinaison d'un senseur d'étoiles et d'un capteur métrologique optique de vol en formation |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19703629A1 (de) * | 1997-01-31 | 1998-08-06 | Daimler Benz Aerospace Ag | Verfahren zur bordautonomen Bestimmung der Position eines Satelliten |
FR2666561B1 (fr) * | 1990-09-06 | 1995-06-09 | Aerospatiale | Procede de pilotage d'un engin spatial dote d'un mouvement de precession et dispositif pour sa mise en óoeuvre. |
FR2691426B1 (fr) * | 1992-05-19 | 1997-09-19 | Aerospatiale | Procede et dispositif d'acquisition de la terre via la polaire pour satellite stabilise 3-axes en orbite de faible inclinaison. |
US5348255A (en) * | 1992-06-02 | 1994-09-20 | Hughes Aircraft Company | System and method for sensing attitude of a spacecraft with equilized star tracker errors along three orthogonal axes |
US5608634A (en) * | 1992-06-12 | 1997-03-04 | Martin Marietta Corp. | Low noise spacecraft body rate sensing arrangement for attitude control |
US5319969A (en) * | 1992-09-21 | 1994-06-14 | Honeywell Inc. | Method for determining 3-axis spacecraft attitude |
US5319968A (en) * | 1992-09-21 | 1994-06-14 | Honeywell Inc. | Apparatus for determining 3-axis space craft attitude |
US5412574A (en) * | 1993-05-14 | 1995-05-02 | Hughes Aircraft Company | Method of attitude determination using earth and star sensors |
US5852792A (en) * | 1996-10-03 | 1998-12-22 | Lockheed Martin Corporation | Spacecraft boresight calibration filter |
US6216983B1 (en) * | 1999-06-29 | 2001-04-17 | Trw Inc. | Ephemeris/attitude reference determination using communications links |
US6142423A (en) * | 1999-06-29 | 2000-11-07 | Trw Inc. | Ephemeris/attitude reference determination using on-board optics and other satellite ephemeris |
US6360996B1 (en) * | 2000-02-24 | 2002-03-26 | Hughes Electronics Corporation | Steering control for skewed scissors pair CMG clusters |
AU2002251827A1 (en) | 2001-01-26 | 2002-08-06 | The Charles Stark Draper Laboratory, Inc. | Miniature attitude sensing suite |
US7878429B2 (en) * | 2007-09-28 | 2011-02-01 | Lindsay Corporation | Solar powered irrigation machine |
US8218013B1 (en) * | 2008-05-27 | 2012-07-10 | Exelis, Inc | Star sensing for an earth imaging sensor |
US8222582B1 (en) * | 2008-09-30 | 2012-07-17 | Anderson Mark J | Celestial navigation using stellar narrow-band emission |
US8433515B2 (en) * | 2011-07-06 | 2013-04-30 | Tsinghua University | Method for measuring precision of star sensor and system using the same |
CN103344872B (zh) * | 2013-06-28 | 2015-11-18 | 上海新跃仪表厂 | 一种星敏安装极性的测试方法 |
CN103323031B (zh) * | 2013-06-28 | 2015-11-18 | 上海新跃仪表厂 | 一种基于星敏的地平仪系统误差在线补偿的方法 |
EP2879011B1 (en) * | 2013-12-02 | 2021-02-03 | Airbus Defence and Space GmbH | On-board estimation of the nadir attitude of an Earth orbiting spacecraft |
CN104833359B (zh) * | 2015-05-27 | 2016-06-15 | 北京航空航天大学 | 一种基于离散马尔科夫特征序列模型的星图模式识别方法 |
CN106382927B (zh) * | 2016-08-19 | 2019-10-18 | 哈尔滨工业大学 | 一种基于卫星识别的星敏感器自主导航方法 |
CN107121707B (zh) * | 2017-05-09 | 2018-12-25 | 深圳清华大学研究院 | 一种三轴磁传感器测量基准与结构基准的误差校正方法 |
US10538342B2 (en) | 2017-05-23 | 2020-01-21 | Space Systems/Loral, Llc | Ecliptic sun acquisition control mode for satellites |
CN108364279B (zh) * | 2017-12-26 | 2020-06-05 | 中国人民解放军战略支援部队信息工程大学 | 确定静止轨道遥感卫星指向偏差的方法 |
CN112093080B (zh) * | 2020-09-22 | 2022-06-24 | 上海航天控制技术研究所 | 倾斜轨道卫星平台控制方法、电子设备及存储介质 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2532911A1 (fr) * | 1982-09-09 | 1984-03-16 | Centre Nat Etd Spatiales | Procede pour la correction d'orbite d'un satellite artificiel et dispositif correspondant |
FR2568680A1 (fr) * | 1984-08-03 | 1986-02-07 | Messerschmitt Boelkow Blohm | Dispositif de mesure pour determiner la position d'un satellite de la terre. |
EP0174715A2 (en) * | 1984-09-13 | 1986-03-19 | Mitsubishi Denki Kabushiki Kaisha | Attitude angle calculation apparatus for a geostationary satellite |
EP0363243A1 (fr) * | 1988-10-06 | 1990-04-11 | AEROSPATIALE Société Nationale Industrielle | Procédé et système de contrôle autonome d'orbite d'un satellite géostationnaire |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4114841A (en) * | 1977-02-22 | 1978-09-19 | Rca Corporation | Magnetic torquing system for changing the spin rate of an orbiting satellite |
US4617634A (en) * | 1983-06-28 | 1986-10-14 | Mitsubishi Denki Kabushiki Kaisha | Artificial satellite attitude control system |
JPS60104499A (ja) * | 1983-11-11 | 1985-06-08 | 株式会社日立製作所 | 姿勢決定方式 |
US4837699A (en) * | 1985-07-18 | 1989-06-06 | Hughes Aircraft Company | Method for controlling the spin axis attitude of a spinning spacecraft |
US4746976A (en) * | 1986-05-23 | 1988-05-24 | Ford Aerospace & Communications Corporation | Star sightings by satellite for image navigation |
US4827422A (en) * | 1986-12-04 | 1989-05-02 | Barnes Engineering Company | Fan scan horizon sensor for a spin stabilized satellite |
US4916622A (en) * | 1988-06-16 | 1990-04-10 | General Electric Company | Attitude control system |
USH712H (en) * | 1988-08-03 | 1989-11-07 | The United States Of America As Represented By The Secretary Of The Army | Method of stellar navigation using an optical correlator |
US5012081A (en) * | 1989-06-22 | 1991-04-30 | Northrop Corporation | Strapdown stellar sensor and holographic lens therefor |
-
1990
- 1990-04-19 US US07/511,169 patent/US5107434A/en not_active Expired - Fee Related
-
1991
- 1991-04-05 FR FR9104157A patent/FR2661261A1/fr active Granted
- 1991-04-16 JP JP3109535A patent/JPH04228400A/ja not_active Withdrawn
- 1991-04-16 DE DE4112361A patent/DE4112361A1/de not_active Withdrawn
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2532911A1 (fr) * | 1982-09-09 | 1984-03-16 | Centre Nat Etd Spatiales | Procede pour la correction d'orbite d'un satellite artificiel et dispositif correspondant |
FR2568680A1 (fr) * | 1984-08-03 | 1986-02-07 | Messerschmitt Boelkow Blohm | Dispositif de mesure pour determiner la position d'un satellite de la terre. |
EP0174715A2 (en) * | 1984-09-13 | 1986-03-19 | Mitsubishi Denki Kabushiki Kaisha | Attitude angle calculation apparatus for a geostationary satellite |
EP0363243A1 (fr) * | 1988-10-06 | 1990-04-11 | AEROSPATIALE Société Nationale Industrielle | Procédé et système de contrôle autonome d'orbite d'un satellite géostationnaire |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2050674A1 (fr) * | 2007-10-19 | 2009-04-22 | Thales | Système de visée absolue améliorée par combinaison d'un senseur d'étoiles et d'un capteur métrologique optique de vol en formation |
FR2922659A1 (fr) * | 2007-10-19 | 2009-04-24 | Thales Sa | Systeme de visee absolue amelioree par combinaison d'un senseur d'etoiles et d'un capteur metrologique optique de vol en formation |
US7745768B2 (en) | 2007-10-19 | 2010-06-29 | Thales | Absolute target system enhanced by combining a star sensor and a formation flight optical metrological sensor |
Also Published As
Publication number | Publication date |
---|---|
FR2661261B1 (US06826419-20041130-M00005.png) | 1995-01-20 |
US5107434A (en) | 1992-04-21 |
JPH04228400A (ja) | 1992-08-18 |
DE4112361A1 (de) | 1991-10-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property | ||
ST | Notification of lapse |
Effective date: 20081231 |