DE69002449T2 - System zur Steuerung der Lage eines stabilisierten Satelliten durch Solarzellen. - Google Patents

System zur Steuerung der Lage eines stabilisierten Satelliten durch Solarzellen.

Info

Publication number
DE69002449T2
DE69002449T2 DE90403721T DE69002449T DE69002449T2 DE 69002449 T2 DE69002449 T2 DE 69002449T2 DE 90403721 T DE90403721 T DE 90403721T DE 69002449 T DE69002449 T DE 69002449T DE 69002449 T2 DE69002449 T2 DE 69002449T2
Authority
DE
Germany
Prior art keywords
controlling
solar cells
stabilized satellite
satellite
stabilized
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 - Fee Related
Application number
DE90403721T
Other languages
English (en)
Other versions
DE69002449D1 (de
Inventor
Patrick Flament
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
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Publication of DE69002449D1 publication Critical patent/DE69002449D1/de
Application granted granted Critical
Publication of DE69002449T2 publication Critical patent/DE69002449T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/407—Solar sailing
    • 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
    • B64G1/363—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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S136/00—Batteries: thermoelectric and photoelectric
    • Y10S136/291—Applications
    • Y10S136/292—Space - satellite
DE90403721T 1989-12-29 1990-12-20 System zur Steuerung der Lage eines stabilisierten Satelliten durch Solarzellen. Expired - Fee Related DE69002449T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8917479A FR2656586B1 (fr) 1989-12-29 1989-12-29 Dispositif de controle d'attitude par voiles solaires pour satellite stabilise autour de trois axes.

Publications (2)

Publication Number Publication Date
DE69002449D1 DE69002449D1 (de) 1993-09-02
DE69002449T2 true DE69002449T2 (de) 1993-11-18

Family

ID=9389165

Family Applications (1)

Application Number Title Priority Date Filing Date
DE90403721T Expired - Fee Related DE69002449T2 (de) 1989-12-29 1990-12-20 System zur Steuerung der Lage eines stabilisierten Satelliten durch Solarzellen.

Country Status (6)

Country Link
US (1) US5133518A (de)
EP (1) EP0436425B1 (de)
CA (1) CA2032808C (de)
DE (1) DE69002449T2 (de)
ES (1) ES2042251T3 (de)
FR (1) FR2656586B1 (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5257759A (en) * 1991-11-27 1993-11-02 Hughes Aircraft Company Method and apparatus for controlling a solar wing of a satellite using a sun sensor
US5618012A (en) * 1995-01-12 1997-04-08 Space Systems/Loral, Inc. Satellite stabilization system
US5765780A (en) * 1995-12-22 1998-06-16 Hughes Electronics Corporation Systematic vectored thrust calibration method for satellite momentum control
US5816540A (en) * 1995-12-22 1998-10-06 Hughes Electronics Optimal solar tracking system
US5996942A (en) * 1996-10-16 1999-12-07 Space Systems/Loral, Inc. Autonomous solar torque management
US5906339A (en) * 1996-11-07 1999-05-25 Motorola, Inc. Multiple axis solar sailing
US6003817A (en) * 1996-11-12 1999-12-21 Motorola, Inc. Actively controlled thermal panel and method therefor
FR2765189B1 (fr) * 1997-06-25 1999-08-20 Agence Spatiale Europeenne Dispositif de stabilisation passive de la direction de pointage d'un engin spatial
EP0945343A1 (de) * 1998-03-26 1999-09-29 Fokker Space B.V. System zur kinematischen Verbindung von benachbarten Paneelen in einer Paneelanordnung
US6227497B1 (en) * 1998-08-19 2001-05-08 Mobile Communications Holdings, Inc. Adaptively positioned solar array
US6019320A (en) * 1998-09-15 2000-02-01 Hughes Electronics Corporation Spacecraft acquisition of sun pointing
US6373023B1 (en) 1999-03-02 2002-04-16 General Dynamics (Ots) Aerospace, Inc. ARC discharge initiation for a pulsed plasma thruster
DE10103074A1 (de) * 2001-01-24 2002-08-01 Eurocopter Deutschland Tragstruktur für ein Sonnensegel eines Satelliten
FR2846298A1 (fr) * 2002-10-29 2004-04-30 Cit Alcatel Ensemble articule de panneaux de generateur solaire et vehicule spatial
FR2848529B1 (fr) * 2002-12-12 2005-02-25 Astrium Sas Procede de pilotage solaire de vehicule spatial
US7104506B1 (en) * 2003-08-06 2006-09-12 Lockheed Martin Corporation Spacecraft disturbance trimming system
KR100573876B1 (ko) * 2004-07-13 2006-04-25 한국과학기술원 태양 복사 압력을 이용하여 타원 궤도에 있는 위성 자세제어 방법
US7980514B2 (en) * 2008-03-14 2011-07-19 Northrop Grumman Space & Mission Systems Corp. Solar array momentum control
US8090484B1 (en) * 2009-03-12 2012-01-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Orientation control method and system for object in motion
FR2970701B1 (fr) * 2011-01-25 2015-04-17 Astrium Sas Dispositif de controle d'attitude d'un satellite et procede de commande d'un satellite embarquant ledit dispositif
US8868263B2 (en) 2011-05-25 2014-10-21 Space Systems/Loral, Llc Spacecraft momentum management using solar array
FR2980176A1 (fr) * 2011-09-19 2013-03-22 Astrium Sas Procede de controle d'attitude d'un satellite et satellite commande en attitude
JP2015074376A (ja) * 2013-10-10 2015-04-20 三菱重工業株式会社 人工衛星及び合成開口レーダー
US10647450B2 (en) * 2016-03-18 2020-05-12 The Boeing Company Satellite control system using electrically controllable variable reflection glass panels
CN110963087B (zh) * 2019-11-11 2021-10-29 上海航天控制技术研究所 一种多模式复杂流程的空间站太阳翼的控制方法
CN116674769B (zh) * 2023-06-08 2024-01-30 重庆开拓卫星科技有限公司 一种太阳翼多自由度驱动装置

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3304028A (en) * 1964-08-11 1967-02-14 Hugh L Dryden Attitude control for spacecraft
US3339863A (en) * 1965-09-16 1967-09-05 James E Webb Solar vane actuator
DE2537577A1 (de) * 1975-08-22 1977-03-03 Michael Dipl Ing Truemper Lagerregelung fuer satelliten
DE2604005A1 (de) * 1976-02-03 1977-08-11 Messerschmitt Boelkow Blohm Einrichtung zur beeinflussung der position und lage eines satelliten
FR2513589A1 (fr) * 1981-09-28 1983-04-01 Aerospatiale Procede et dispositif pour aligner l'axe de roulis d'un satellite avec une direction desiree
FR2530046A1 (fr) * 1982-07-06 1984-01-13 Matra Procede et dispositif de commande d'attitude pour satellite geosynchrone
JPS6486498A (en) * 1987-09-28 1989-03-31 Shimadzu Corp Continuous photographing system in capacitor type x-ray device
JPH03503270A (ja) * 1988-12-02 1991-07-25 インスティテュト　コスミチェスキヒ　イススレドバニ　アカデミイ　ナウク　エスエスエスエル 宇宙船
DE3907063A1 (de) * 1989-03-04 1990-09-13 Messerschmitt Boelkow Blohm Solargeneratoranordnung fuer teil- und vollentfaltung

Also Published As

Publication number Publication date
CA2032808A1 (en) 1991-06-30
DE69002449D1 (de) 1993-09-02
ES2042251T3 (es) 1993-12-01
CA2032808C (en) 2000-03-21
EP0436425A1 (de) 1991-07-10
US5133518A (en) 1992-07-28
FR2656586A1 (fr) 1991-07-05
EP0436425B1 (de) 1993-07-28
FR2656586B1 (fr) 1992-05-07

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee