ES2043056T3 - Procedimiento de observacion por barrido de un cuerpo celeste y de medida de una velocidad angular de un vehiculo espacial, sistema de observacion para su puesta en practica, y vehiculo espacial que lo contiene. - Google Patents

Procedimiento de observacion por barrido de un cuerpo celeste y de medida de una velocidad angular de un vehiculo espacial, sistema de observacion para su puesta en practica, y vehiculo espacial que lo contiene.

Info

Publication number
ES2043056T3
ES2043056T3 ES89401210T ES89401210T ES2043056T3 ES 2043056 T3 ES2043056 T3 ES 2043056T3 ES 89401210 T ES89401210 T ES 89401210T ES 89401210 T ES89401210 T ES 89401210T ES 2043056 T3 ES2043056 T3 ES 2043056T3
Authority
ES
Spain
Prior art keywords
space vehicle
observation
sweeping
angular speed
celestial body
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
Application number
ES89401210T
Other languages
English (en)
Inventor
Herve Sainct
Patrick Maute
Jean-Francois Plantier
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=9365796&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=ES2043056(T3) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2043056T3 publication Critical patent/ES2043056T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • G01S3/7868—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 using 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
    • B64G1/36—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
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds
    • G01P3/64—Devices characterised by the determination of the time taken to traverse a fixed distance
    • G01P3/68—Devices characterised by the determination of the time taken to traverse a fixed distance using optical means, i.e. using infrared, visible, or ultraviolet light
    • 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
    • B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • Electromagnetism (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Navigation (AREA)
  • Gyroscopes (AREA)

Abstract

PROCEDIMIENTO DE OBSERVACION POR BARRIDO DE UN CUERPO CELESTE (T) A PARTIR DE UN VEHICULO ESPACIAL (5) COMPORTANDO UN SISTEMA DE OBSERVACION POR BARRIDO POR REFERENCIA A UN EJE DE BARRIDO CARACTERIZADO EN QUE SE FORMAN (16) SUCESIVAMENTE DOS SEÑALES (A, B) CORRESPONDIENDO AL BARRIDO, EN UN MISMO SENTIDO DE DESLIZAMIENTO DE UNA MISMA TOMA DE TIERRA (BT), SE DETECTA (17) EN CADA UNA DE ESTAS SEÑALES UNA TRANSICION CARACTERISTICA (A1, B1) REPRESENTATIVA DE UN MISMO PUNTO CARACTERISTICO DE ESTA TOMA DE TIERRA, SE RECOGE (18) LA POSICION RELATIVA DE ESTAS TRANSICIONES EN ESTAS SEÑALES, Y SE DETERMINA (19) A PARTIR DE UN EVENTUAL DISTANCIAMIENTO ENTRE ESTAS POSICIONES RELATIVAS UNA EVENTUAL VELOCIDAD ANGULAR (W) DEL VEHICULO ESPACIAL, TNEIENDO EN CUENTA EL DISTANCIAMIENTO DE TIEMPO SEPARANDO LOS MOMENTOS DONDE CADA UNA DE ESTAS TRANSICIONES HA APARECIDO EN DICHAS SEÑALES.
ES89401210T 1988-04-28 1989-04-27 Procedimiento de observacion por barrido de un cuerpo celeste y de medida de una velocidad angular de un vehiculo espacial, sistema de observacion para su puesta en practica, y vehiculo espacial que lo contiene. Expired - Lifetime ES2043056T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8805708A FR2630705B1 (fr) 1988-04-28 1988-04-28 Procede d'observation par balayage d'un corps celeste et de mesure d'une vitesse angulaire d'un vehicule spatial, systeme d'observation pour sa mise en oeuvre, et vehicule spatial le comportant

Publications (1)

Publication Number Publication Date
ES2043056T3 true ES2043056T3 (es) 1993-12-16

Family

ID=9365796

Family Applications (1)

Application Number Title Priority Date Filing Date
ES89401210T Expired - Lifetime ES2043056T3 (es) 1988-04-28 1989-04-27 Procedimiento de observacion por barrido de un cuerpo celeste y de medida de una velocidad angular de un vehiculo espacial, sistema de observacion para su puesta en practica, y vehiculo espacial que lo contiene.

Country Status (7)

Country Link
US (1) US5062051A (es)
EP (1) EP0341142B1 (es)
JP (1) JP2740920B2 (es)
CA (1) CA1326529C (es)
DE (1) DE68907440T2 (es)
ES (1) ES2043056T3 (es)
FR (1) FR2630705B1 (es)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2653918B1 (fr) * 1989-10-31 1992-02-14 Europ Agence Spatiale Procede de rectification en temps reel des images des satellites meteorologiques geostationnaires.
US5257760A (en) * 1992-06-24 1993-11-02 Edo Corporation, Barnes Engineering Division Scanning earth sensor using the sun's position for determining yaw
US5546309A (en) * 1993-10-20 1996-08-13 The Charles Stark Draper Laboratory, Inc. Apparatus and method for autonomous satellite attitude sensing
US6732977B1 (en) 2002-02-11 2004-05-11 Lockheed Martin Corporation System for on-orbit correction of spacecraft payload pointing errors
US6695263B1 (en) * 2002-02-12 2004-02-24 Lockheed Martin Corporation System for geosynchronous spacecraft rapid earth reacquisition
US7051980B2 (en) * 2002-02-26 2006-05-30 Lockheed Martin Corporation Efficient orbit sparing system for space vehicle constellations
US6702234B1 (en) 2002-03-29 2004-03-09 Lockheed Martin Corporation Fault tolerant attitude control system for zero momentum spacecraft
US7835826B1 (en) 2005-12-13 2010-11-16 Lockheed Martin Corporation Attitude determination system for yaw-steering spacecraft
JP4820976B2 (ja) * 2006-10-06 2011-11-24 株式会社指月電機製作所 トランスコアの固定構造
US8767072B1 (en) * 2010-03-26 2014-07-01 Lockheed Martin Corporation Geoposition determination by starlight refraction measurement
CN106225807A (zh) * 2016-07-27 2016-12-14 中国科学院长春光学精密机械与物理研究所 视频卫星对地面区域目标进行凝视成像的仿真方法及系统
US10612901B2 (en) * 2018-03-23 2020-04-07 Simmonds Precision Products, Inc. Real-time compensation of inertial gyroscopes
CN111897357B (zh) * 2020-08-13 2023-10-20 上海航天控制技术研究所 一种卫星对地扫描的姿态跟踪控制方法

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA633497A (en) * 1961-12-26 Collins Radio Company Satellite apparent position computer
US2998529A (en) * 1958-06-19 1961-08-29 Kollsman Instr Corp Automatic astrocompass
US3012728A (en) * 1958-07-23 1961-12-12 Collins Radio Co Satellite apparent position computer
US3216674A (en) * 1959-06-08 1965-11-09 Walter G Finch Proportional navigation system for a spinning body in free space
US3310982A (en) * 1961-08-31 1967-03-28 United Aircraft Corp Navigation system with vehicle motion signals modified by drift angle signals
US3576999A (en) * 1965-01-16 1971-05-04 Bendix Corp Method and apparatus for determining the orientation of an object relative to an elliptic object
US3535521A (en) * 1966-02-28 1970-10-20 Itt Satellite attitude control utilizing a plurality of infrared sensors
US3769710A (en) * 1969-04-01 1973-11-06 R Reister Electronic celestial navigation means
JPS4829075B1 (es) 1969-07-25 1973-09-06
FR2246843B1 (es) * 1973-10-04 1976-05-14 Sodern
US4328421A (en) * 1980-02-25 1982-05-04 Barnes Engineering Company Horizon sensor
US4617634A (en) * 1983-06-28 1986-10-14 Mitsubishi Denki Kabushiki Kaisha Artificial satellite attitude control system
JPS6025900A (ja) * 1983-07-25 1985-02-08 株式会社日立製作所 スタ−センサによる姿勢決定システム
DE3330861A1 (de) * 1983-08-26 1985-03-14 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zur feststellung von lageaenderungen eines raumflugkoerpers
JPS60104499A (ja) * 1983-11-11 1985-06-08 株式会社日立製作所 姿勢決定方式
DE3422007C2 (de) * 1984-06-14 1986-10-02 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Anordnung für einen Erdhorizontsensor eines in einem Orbit befindlichen Erdsatelliten
US4628206A (en) 1984-08-27 1986-12-09 Barnes Engineering Company Visible-UV horizon sensor
US4837699A (en) * 1985-07-18 1989-06-06 Hughes Aircraft Company Method for controlling the spin axis attitude of a spinning spacecraft
US4801202A (en) * 1985-12-20 1989-01-31 Itt Aerospace Optical Method and apparatus for radiometer star sensing
SE461835B (sv) * 1986-02-13 1990-04-02 Sparring Elfa Ab Hjulfaeste foer monterbara moebeldelar
US4688092A (en) * 1986-05-06 1987-08-18 Ford Aerospace & Communications Corporation Satellite camera image navigation
US4827422A (en) * 1986-12-04 1989-05-02 Barnes Engineering Company Fan scan horizon sensor for a spin stabilized satellite
US4912475A (en) * 1987-03-20 1990-03-27 Massachusetts Institute Of Technology Techniques for determining orbital data
FR2615477B1 (fr) * 1987-05-22 1989-08-18 Centre Nat Etd Spatiales Dispositif et procede de pointage d'une sonde spatiale vers un corps celeste
US4944587A (en) * 1988-03-17 1990-07-31 Kabushiki Kaisha Toshiba Star sensor
GB8809247D0 (en) * 1988-04-20 1988-05-25 British Aerospace Attitude recovery for spacecraft

Also Published As

Publication number Publication date
CA1326529C (en) 1994-01-25
US5062051A (en) 1991-10-29
EP0341142B1 (fr) 1993-07-07
EP0341142A3 (en) 1989-11-15
FR2630705B1 (fr) 1990-08-24
FR2630705A1 (fr) 1989-11-03
DE68907440T2 (de) 1993-11-04
DE68907440D1 (de) 1993-08-12
JPH0249111A (ja) 1990-02-19
JP2740920B2 (ja) 1998-04-15
EP0341142A2 (fr) 1989-11-08

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