ES2135016T3 - Procedimiento adaptativo de control de posicion para estabilizar magneticamente un satelite en al menos balanceo-guiñada. - Google Patents

Procedimiento adaptativo de control de posicion para estabilizar magneticamente un satelite en al menos balanceo-guiñada.

Info

Publication number
ES2135016T3
ES2135016T3 ES95400503T ES95400503T ES2135016T3 ES 2135016 T3 ES2135016 T3 ES 2135016T3 ES 95400503 T ES95400503 T ES 95400503T ES 95400503 T ES95400503 T ES 95400503T ES 2135016 T3 ES2135016 T3 ES 2135016T3
Authority
ES
Spain
Prior art keywords
satellite
wink
balance
position control
control procedure
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
ES95400503T
Other languages
English (en)
Spanish (es)
Inventor
Bruno Celerier
Francis Douillet
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.)
Alcatel Lucent SAS
Nokia Inc
Original Assignee
Alcatel SA
Nokia Inc
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 Alcatel SA, Nokia Inc filed Critical Alcatel SA
Application granted granted Critical
Publication of ES2135016T3 publication Critical patent/ES2135016T3/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
    • B64G1/244—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
    • B64G1/32—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)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Environmental & Geological Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)
ES95400503T 1994-03-11 1995-03-09 Procedimiento adaptativo de control de posicion para estabilizar magneticamente un satelite en al menos balanceo-guiñada. Expired - Lifetime ES2135016T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9402852A FR2717149B1 (fr) 1994-03-11 1994-03-11 Procédé adaptatif de contrôle d'attitude pour stabiliser magnétiquement un satellite au moins en roulis-lacet.

Publications (1)

Publication Number Publication Date
ES2135016T3 true ES2135016T3 (es) 1999-10-16

Family

ID=9460940

Family Applications (1)

Application Number Title Priority Date Filing Date
ES95400503T Expired - Lifetime ES2135016T3 (es) 1994-03-11 1995-03-09 Procedimiento adaptativo de control de posicion para estabilizar magneticamente un satelite en al menos balanceo-guiñada.

Country Status (11)

Country Link
EP (1) EP0671323B1 (enExample)
JP (1) JPH08510426A (enExample)
KR (1) KR960702400A (enExample)
BR (1) BR9505859A (enExample)
DE (1) DE69509944T2 (enExample)
ES (1) ES2135016T3 (enExample)
FR (1) FR2717149B1 (enExample)
IL (1) IL112912A0 (enExample)
TW (1) TW306898B (enExample)
WO (1) WO1995024340A1 (enExample)
ZA (1) ZA952028B (enExample)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IL126210A (en) * 1998-07-01 2002-12-01 Israel Aircraft Ind Ltd Lightweight and low-excitation magnetoturker
DE19924908B4 (de) * 1999-05-31 2008-05-29 Astrium Gmbh Verfahren zur dreiachsigen Lagebestimmung für einen niedrig fliegenden Satelliten
RU2168188C1 (ru) * 2000-05-26 2001-05-27 Смирнов Борис Михайлович Способ определения проекций вектора магнитной индукции геомагнитного поля с подвижного объекта (варианты)
FR2809502B1 (fr) * 2000-05-29 2002-08-16 Matra Marconi Space France Procede de commande d'attitude d'un satellite en orbite terrestre basse
RU2197013C2 (ru) * 2000-11-09 2003-01-20 Государственное предприятие "Научно-исследовательский институт электрофизической аппаратуры им. Д.В.Ефремова" Способ и следящая система для определения положения и ориентации подвижного объекта
DE60117742T2 (de) * 2001-10-19 2006-11-16 Eads Astrium S.A.S. Verfahren zur Lagesteuerung eines Satelliten auf einer niedrigen Umlaufbahn
RU2204851C1 (ru) * 2001-11-30 2003-05-20 Смирнов Борис Михайлович Устройство для определения индукции геомагнитного поля с подвижного объекта
RU2206109C1 (ru) * 2002-01-31 2003-06-10 Смирнов Борис Михайлович Устройство для определения индукции геомагнитного поля с подвижного объекта
RU2207599C1 (ru) * 2002-07-22 2003-06-27 Смирнов Борис Михайлович Устройство для определения индукции геомагнитного поля с подвижного объекта
RU2236029C1 (ru) * 2003-06-02 2004-09-10 Смирнов Борис Михайлович Устройство для определения индукции геомагнитного поля с подвижного объекта
RU2241958C9 (ru) * 2003-12-02 2005-06-10 Федеральное государственное унитарное предприятие "Научно-исследовательский институт электрофизической аппаратуры им. Д.В.Ефремова" Способ (варианты) и следящая система для определения положения и ориентации подвижного объекта
RU2247404C1 (ru) * 2004-01-19 2005-02-27 Смирнов Борис Михайлович Устройство для определения параметров, характеризующих намагниченность подвижного объекта
RU2257594C1 (ru) * 2004-03-01 2005-07-27 Смирнов Борис Михайлович Устройство для определения параметров, характеризующих намагниченность подвижного объекта
RU2261456C1 (ru) * 2004-05-17 2005-09-27 Смирнов Борис Михайлович Способ определения параметров, характеризующих намагниченность объекта, и устройство для его осуществления
CN116500902B (zh) * 2023-06-27 2023-09-29 航天科工火箭技术有限公司 去任务化姿态控制回路设计方法、存储介质及电子设备

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2080612A1 (en) * 1991-11-27 1993-05-28 Douglas J. Bender Method and apparatus for compensating for magnetic disturbance torques on a satellite

Also Published As

Publication number Publication date
WO1995024340A1 (fr) 1995-09-14
EP0671323B1 (fr) 1999-06-02
FR2717149B1 (fr) 1996-05-31
DE69509944D1 (de) 1999-07-08
KR960702400A (ko) 1996-04-27
ZA952028B (en) 1995-12-11
TW306898B (enExample) 1997-06-01
IL112912A0 (en) 1995-06-29
JPH08510426A (ja) 1996-11-05
BR9505859A (pt) 1996-02-21
DE69509944T2 (de) 2001-07-26
EP0671323A1 (fr) 1995-09-13
FR2717149A1 (fr) 1995-09-15

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