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ES2163602T3 - Procedimiento de mando de posicion de un satelite en orbita baja, con adquisicion solar. - Google Patents

Procedimiento de mando de posicion de un satelite en orbita baja, con adquisicion solar.

Info

Publication number
ES2163602T3
ES2163602T3 ES96402613T ES96402613T ES2163602T3 ES 2163602 T3 ES2163602 T3 ES 2163602T3 ES 96402613 T ES96402613 T ES 96402613T ES 96402613 T ES96402613 T ES 96402613T ES 2163602 T3 ES2163602 T3 ES 2163602T3
Authority
ES
Spain
Prior art keywords
satellite
low orbit
magnetic field
procedure
solar
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
ES96402613T
Other languages
English (en)
Inventor
Patrice Damilano
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 Defence and Space SAS
Original Assignee
Astrium 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
Application filed by Astrium SAS filed Critical Astrium SAS
Application granted granted Critical
Publication of ES2163602T3 publication Critical patent/ES2163602T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B64G1/363—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
    • B64G1/244—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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Measuring Magnetic Variables (AREA)

Abstract

PARA CONTROLAR EL COMPORTAMIENTO DE UN SATELITE COLOCADO EN UNA ORBITA BAJA (10), SE MIDE EL CAMPO MAGNETICO TERRESTRE SEGUN LOS TRES EJES DE UN PUNTO DE REFERENCIA ASOCIADO AL SATELITE, SE DERIVAN LAS MEDICIONES RESPECTO AL TIEMPO, SE MULTIPLICAN LAS DERIVADAS POR UNA GANANCIA Y SE HACE PASAR UNA CORRIENTE REPRESENTATIVA DEL RESULTADO EN MAGNETOACOPLADORES PARA CREAR MOMENTOS MAGNETICOS QUE TIENDEN A MANTENER EL SATELITE EN UNA ORIENTACION INVARIABLE RESPECTO DE LAS LINEAS DE FUERZA DEL CAMPO MAGNETICO TERRESTRE. FUERA DE LOS PERIODOS DE ECLIPSE, SE CONTROL EN CABECEO EL SATELITE POR MODIFICACION DEL MOMENTO DE INERCIA INTERNA EN RESPUESTA A UNA SEÑAL EMITIDA POR UN DETECTOR SOLAR (46), DE MANERA QUE MANTENGA GENERADORES SOLARES (36) QUE LLEVA ORIENTADOS HACIA EL SOL, PARA LAS ORBITAS QUE LLEVAN NUDOS CERCANOS A MEDIODIA Y A MEDIANOCHE EN HORA LOCAL TERRESTRE.
ES96402613T 1995-12-06 1996-12-03 Procedimiento de mando de posicion de un satelite en orbita baja, con adquisicion solar. Expired - Lifetime ES2163602T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9514418A FR2742243B1 (fr) 1995-12-06 1995-12-06 Procede de commande d'attitude d'un satellite en orbite basse, a acquisition solaire

Publications (1)

Publication Number Publication Date
ES2163602T3 true ES2163602T3 (es) 2002-02-01

Family

ID=9485195

Family Applications (1)

Application Number Title Priority Date Filing Date
ES96402613T Expired - Lifetime ES2163602T3 (es) 1995-12-06 1996-12-03 Procedimiento de mando de posicion de un satelite en orbita baja, con adquisicion solar.

Country Status (6)

Country Link
US (1) US5788188A (es)
EP (1) EP0778201B1 (es)
CA (1) CA2192050C (es)
DE (1) DE69615318T2 (es)
ES (1) ES2163602T3 (es)
FR (1) FR2742243B1 (es)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2748721A1 (fr) * 1996-05-17 1997-11-21 Matra Marconi Space France Appareil de reglage de la rotation d'un vaisseau spatial autour d'un axe
US6496741B1 (en) 1999-03-25 2002-12-17 Gregory J. Whiffen Static/dynamic control for optimizing a useful objective
DE19924908B4 (de) * 1999-05-31 2008-05-29 Astrium Gmbh Verfahren zur dreiachsigen Lagebestimmung für einen niedrig fliegenden Satelliten
US6471161B1 (en) 1999-12-27 2002-10-29 Lockheed Martin Corporation Satellite attitude control system
FR2809502B1 (fr) * 2000-05-29 2002-08-16 Matra Marconi Space France Procede de commande d'attitude d'un satellite en orbite terrestre basse
US6481671B1 (en) 2000-08-14 2002-11-19 Ball Aerospace & Technologies Corp. Spacecraft sunshield for use in performing solar torque balancing
FR2815730B1 (fr) * 2000-10-19 2003-10-24 Astrium Sas Procede de commande d'attitude et de stabilisation d'un satellite en orbite basse, par couplage avec le champ magnetique terrestre
WO2002058992A2 (en) 2001-01-26 2002-08-01 The Charles Stark Draper Laboratory, Inc. Miniature attitude sensing suite
EP1308813B8 (fr) * 2001-10-19 2017-05-31 Eads Astrium Sas Procédé de commande d'attitude d'un satellite en orbite terrestre basse
DE60117744T2 (de) * 2001-11-20 2006-11-16 Eads Astrium S.A.S. Steuerungsverfahren zur Lageregelung und Stabilisierung eines Satelliten in niedriger Umlaufbahn, durch Kopplung mit dem Erdmagnetfeld
US6634603B2 (en) * 2001-11-29 2003-10-21 The Boeing Company Magnetic dipole tractor beam control system
US6561462B1 (en) * 2002-02-21 2003-05-13 The Boeing Company Spacecraft power/sun aquistion algorithm using slit sun sensors
US6745984B2 (en) 2002-04-23 2004-06-08 Astrium Sas Method of controlling the attitude and stabilization of a satellite in low orbit
US8403270B2 (en) * 2006-09-15 2013-03-26 The Boeing Company Canted solar array and method for using same
CN102431659B (zh) * 2011-10-27 2013-07-24 北京航空航天大学 一种日地系统Halo轨道探测器的构型及其姿态指向
FR3013685B1 (fr) * 2013-11-25 2017-05-19 Astrium Sas Procede et dispositif de commande d'une phase d'acquisition du soleil par un engin spatial
RU2580593C2 (ru) * 2014-06-10 2016-04-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ разгрузки силовых гироскопов космического аппарата с создаваемым магнитным моментом
FR3026858B1 (fr) * 2014-10-02 2016-12-09 Airbus Defence & Space Sas Procede de controle d'attitude d'un satellite en mode survie, satellite adapte et procede de commande a distance d'un tel satellite
FR3093326B1 (fr) * 2019-03-01 2024-10-04 Centre Nat Etd Spatiales Procédé de contrôle de l’attitude d’un satellite en orbite basse
FR3093998B1 (fr) * 2019-03-20 2021-09-10 Airbus Defence & Space Sas Procédé de contrôle d’attitude d’un satellite en mode survie sans connaissance a priori de l’heure locale de l’orbite du satellite
US11338944B2 (en) 2019-05-29 2022-05-24 GM Global Technology Operations LLC Control system for executing a safing mode sequence in a spacecraft
US11174047B2 (en) 2019-05-29 2021-11-16 The Boeing Company Spacecraft control system for determining reaction torque
US11273933B2 (en) * 2019-05-29 2022-03-15 The Boeing Company Spacecraft attitude control strategy for reducing disturbance torques
CN111874269B (zh) * 2020-08-10 2022-02-01 吉林大学 一种磁控小卫星的低功耗对日捕获及定向姿态控制方法
CN113353292B (zh) * 2021-06-26 2022-06-07 山东航天电子技术研究所 磁控非自旋对日定向方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1088653A (en) * 1975-09-15 1980-10-28 George E. Schmidt, Jr. Magnetic control of spacecraft roll disturbance torques
US4071211A (en) * 1976-09-23 1978-01-31 Rca Corporation Momentum biased active three-axis satellite attitude control system
US5123617A (en) * 1990-03-05 1992-06-23 General Electric Company Spacecraft momentum unloading using controlled magnetic torques
CA2080612A1 (en) * 1991-11-27 1993-05-28 Douglas J. Bender Method and apparatus for compensating for magnetic disturbance torques on a satellite
US5337981A (en) * 1991-11-27 1994-08-16 Hughes Aircraft Company Method and apparatus for compensating for solar torque transients on a satellite during a solar eclipse
US5248118A (en) * 1992-05-13 1993-09-28 General Electric Co. Spacecraft attitude control system with reaction wheel bearing protection
FR2710314B1 (fr) * 1993-09-23 1995-12-15 Aerospatiale Satellite stabilisé 3-axes à pointage géocentrique en orbite basse à générateur solaire orientable 1-axe.

Also Published As

Publication number Publication date
EP0778201A1 (fr) 1997-06-11
CA2192050A1 (fr) 1997-06-07
DE69615318D1 (de) 2001-10-25
DE69615318T2 (de) 2002-07-04
CA2192050C (fr) 2004-11-23
EP0778201B1 (fr) 2001-09-19
FR2742243B1 (fr) 1998-02-13
US5788188A (en) 1998-08-04
FR2742243A1 (fr) 1997-06-13

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