DE69412211T2 - Verfahren zur Lageerhaltung eines Satelliten - Google Patents

Verfahren zur Lageerhaltung eines Satelliten

Info

Publication number
DE69412211T2
DE69412211T2 DE69412211T DE69412211T DE69412211T2 DE 69412211 T2 DE69412211 T2 DE 69412211T2 DE 69412211 T DE69412211 T DE 69412211T DE 69412211 T DE69412211 T DE 69412211T DE 69412211 T2 DE69412211 T2 DE 69412211T2
Authority
DE
Germany
Prior art keywords
satellite
maintaining
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
DE69412211T
Other languages
English (en)
Other versions
DE69412211D1 (de
Inventor
Bernhard M Anzel
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.)
DirecTV Group Inc
Original Assignee
Hughes Electronics Corp
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 Hughes Electronics Corp filed Critical Hughes Electronics Corp
Application granted granted Critical
Publication of DE69412211D1 publication Critical patent/DE69412211D1/de
Publication of DE69412211T2 publication Critical patent/DE69412211T2/de
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
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE69412211T 1993-11-17 1994-11-17 Verfahren zur Lageerhaltung eines Satelliten Expired - Lifetime DE69412211T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/153,512 US5443231A (en) 1993-11-17 1993-11-17 Method and apparatus for a satellite station keeping

Publications (2)

Publication Number Publication Date
DE69412211D1 DE69412211D1 (de) 1998-09-10
DE69412211T2 true DE69412211T2 (de) 1999-04-22

Family

ID=22547521

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69412211T Expired - Lifetime DE69412211T2 (de) 1993-11-17 1994-11-17 Verfahren zur Lageerhaltung eines Satelliten

Country Status (3)

Country Link
US (1) US5443231A (de)
EP (1) EP0654403B1 (de)
DE (1) DE69412211T2 (de)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5813633A (en) 1995-12-22 1998-09-29 Hughes Electronics Corporation Method and apparatus for stationkeeping a satellite offset by pitch rotation
US5984236A (en) 1995-12-22 1999-11-16 Keitel; Keith F. Momentum unloading using gimbaled thrusters
US5826830A (en) * 1995-12-22 1998-10-27 Hughes Electronics Corporation Dual-half system, full torque reaction control thruster configuration for three-axis stabilized spacecraft
US5765780A (en) * 1995-12-22 1998-06-16 Hughes Electronics Corporation Systematic vectored thrust calibration method for satellite momentum control
US5755406A (en) * 1995-12-22 1998-05-26 Hughes Electronics Modular, independent subsystem design satellite bus and variable communication payload configurations and missions
US5738309A (en) * 1996-02-28 1998-04-14 Hughes Electronics Single axis correction for orbit inclination
US5810295A (en) * 1996-07-10 1998-09-22 Hughes Electronics Corporation Method and apparatus for a satellite station keeping
US5826831A (en) * 1996-08-22 1998-10-27 Hughes Electronics Satellite co-location methods
US5957411A (en) * 1997-01-31 1999-09-28 Space Systems/Loral, Inc. Method using double thruster firings to deadbeat flexible solar array structural oscillations
US6042058A (en) * 1997-04-29 2000-03-28 Hughes Electronics Corporation Stationkeeping and momentum-dumping thruster systems and methods
KR100221559B1 (ko) * 1997-05-15 1999-09-15 정선종 위성의 온보드 자동 제어 방법
US6015116A (en) * 1997-12-11 2000-01-18 Hughes Electronics Corporation Fuel efficient methods for satellite stationkeeping and momentum dumping
US6135394A (en) 1998-12-08 2000-10-24 Space Systems/Loral, Inc. Practical method and apparatus for satellite stationkeeping
US6296207B1 (en) * 1999-01-27 2001-10-02 Space Systems/Loral, Inc. Combined stationkeeping and momentum management
DE10029768A1 (de) * 2000-06-16 2002-01-10 Daimler Chrysler Ag Verfahren zur Positionshaltung von geostationären Satelliten
US6435457B1 (en) 2001-01-25 2002-08-20 The Boeing Company Thruster systems for spacecraft station changing, station keeping and momentum dumping
US8205839B2 (en) * 2006-11-06 2012-06-26 The Boeing Company Methods and apparatus for node-synchronous eccentricity control
US8439312B2 (en) * 2007-07-17 2013-05-14 The Boeing Company System and methods for simultaneous momentum dumping and orbit control
US7918420B2 (en) * 2007-07-17 2011-04-05 The Boeing Company System and methods for simultaneous momentum dumping and orbit control
GB2460443A (en) * 2008-05-29 2009-12-02 Inmarsat Global Ltd Propulsion system arrangement for decommissioning a satellite
FR2980176A1 (fr) * 2011-09-19 2013-03-22 Astrium Sas Procede de controle d'attitude d'un satellite et satellite commande en attitude
US9296494B1 (en) 2012-08-10 2016-03-29 Lockheed Martin Corporation Thruster orbit control method and configuration
US10183765B2 (en) 2014-03-12 2019-01-22 Lockheed Martin Corporation Thruster arrangement for geosynchronous orbit spacecraft
FR3022530B1 (fr) 2014-06-19 2018-03-02 Airbus Defence And Space Sas Procede de controle d'orbite d'un satellite en orbite terrestre, satellite et systeme de controle d'orbite d'un tel satellite
EP3186151B1 (de) 2014-08-26 2020-12-30 Astroscale Israel Ltd. Andocksystem und verfahren für satelliten
EP3243756B1 (de) * 2015-01-09 2020-12-30 Mitsubishi Electric Corporation Umlaufbahnsteuerungsvorrichtung und satellit
IL237081A0 (en) * 2015-02-04 2015-11-30 Israel Aerospace Ind Ltd System and method for satellite maneuvering
FR3032427B1 (fr) 2015-02-10 2017-03-10 Airbus Defence & Space Sas Satellite a moyens de propulsion electriques, procede de mise a poste d'un tel satellite et procede de maintien a poste dudit satellite
US9764859B2 (en) * 2015-06-29 2017-09-19 The Boeing Company Efficient stationkeeping design for mixed fuel systems
US10005568B2 (en) 2015-11-13 2018-06-26 The Boeing Company Energy efficient satellite maneuvering
CN105539881B (zh) * 2015-12-15 2018-02-02 北京理工大学 一种仅使用一对斜对称推力器的位置保持优化方法
CN106184818A (zh) * 2016-03-07 2016-12-07 北京理工大学 地球静止卫星推力器故障工况下轨道位置保持方法
US10569909B2 (en) 2016-03-30 2020-02-25 The Boeing Company Systems and methods for satellite orbit and momentum control
US10625882B2 (en) * 2017-03-06 2020-04-21 Effective Space Solutions Ltd. Service satellite for providing in-orbit services using variable thruster control
CN107487460B (zh) * 2017-06-30 2020-07-14 上海卫星工程研究所 适应多种降交点地方时的遥感卫星构型方法
EP3959142B1 (de) * 2020-07-02 2023-06-07 Airbus Defence and Space SAS Verfahren zur umlaufbahnsteuerung und -desaturation eines satelliten mittels gelenkarmen, die eine antriebseinheit tragen

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3907226A (en) * 1970-07-06 1975-09-23 Hughes Aircraft Co Redundant position and attitude control for spin stabilized devices
US3866025A (en) * 1972-03-17 1975-02-11 Rca Corp Spacecraft attitude control system
US4630790A (en) * 1984-11-19 1986-12-23 Ford Aerospace & Communications Corporation Velocity and attitude control for exoatmospheric projectile
JP2650333B2 (ja) * 1988-06-30 1997-09-03 松下電器産業株式会社 電子楽器のスライド蓋
US5020746A (en) * 1989-09-29 1991-06-04 Hughes Aircraft Company Method for satellite station keeping
FR2661889B1 (fr) * 1990-05-09 1994-09-09 Europ Agence Spatiale Systeme propulsif pour un engin spatial stabilise en rotation et procede de commande de sa mise a feu.
IT1245661B (it) * 1991-01-23 1994-10-06 Selenia Spazio Spa Ora Alenia Satellite stabilizzato a tre assi dotato di propulsori elettrici per manovre orbitali e controllo di assetto.
GB9127433D0 (en) * 1991-12-27 1992-02-19 Matra Marconi Space Uk Propulsion system for spacecraft
US5318256A (en) * 1992-10-05 1994-06-07 Rockwell International Corporation Rocket deceleration system

Also Published As

Publication number Publication date
US5443231A (en) 1995-08-22
EP0654403B1 (de) 1998-08-05
DE69412211D1 (de) 1998-09-10
EP0654403A1 (de) 1995-05-24

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Legal Events

Date Code Title Description
8327 Change in the person/name/address of the patent owner

Owner name: HUGHES ELECTRONICS CORP., EL SEGUNDO, CALIF., US

8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: WITTE, WELLER & PARTNER, 70178 STUTTGART