FR2365154A1 - Procede de regulation d'attitude et de changement d'orbite d'un satellite, notamment geostationnaire, stabilisable suivant trois axes et dispositif de mise en oeuvre dudit procede - Google Patents

Procede de regulation d'attitude et de changement d'orbite d'un satellite, notamment geostationnaire, stabilisable suivant trois axes et dispositif de mise en oeuvre dudit procede

Info

Publication number
FR2365154A1
FR2365154A1 FR7727476A FR7727476A FR2365154A1 FR 2365154 A1 FR2365154 A1 FR 2365154A1 FR 7727476 A FR7727476 A FR 7727476A FR 7727476 A FR7727476 A FR 7727476A FR 2365154 A1 FR2365154 A1 FR 2365154A1
Authority
FR
France
Prior art keywords
satellite
axes
attitude
orbit
stabilizable
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.)
Granted
Application number
FR7727476A
Other languages
English (en)
French (fr)
Other versions
FR2365154B1 (enExample
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 GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2365154A1 publication Critical patent/FR2365154A1/fr
Application granted granted Critical
Publication of FR2365154B1 publication Critical patent/FR2365154B1/fr
Granted 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
    • B64G1/28—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
    • B64G1/244—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
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • 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
    • B64G1/281—Spin-stabilised spacecraft
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR7727476A 1976-09-18 1977-09-12 Procede de regulation d'attitude et de changement d'orbite d'un satellite, notamment geostationnaire, stabilisable suivant trois axes et dispositif de mise en oeuvre dudit procede Granted FR2365154A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2642061A DE2642061C2 (de) 1976-09-18 1976-09-18 Lageregelungs- und Bahnänderungsverfahren für einen dreiachsenstabilisierbaren Satelliten, insbesondere für einen geostationären Satelliten und Einrichtung zur Durchführung des Verfahrens

Publications (2)

Publication Number Publication Date
FR2365154A1 true FR2365154A1 (fr) 1978-04-14
FR2365154B1 FR2365154B1 (enExample) 1981-05-08

Family

ID=5988259

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7727476A Granted FR2365154A1 (fr) 1976-09-18 1977-09-12 Procede de regulation d'attitude et de changement d'orbite d'un satellite, notamment geostationnaire, stabilisable suivant trois axes et dispositif de mise en oeuvre dudit procede

Country Status (4)

Country Link
US (1) US4288051A (enExample)
DE (1) DE2642061C2 (enExample)
FR (1) FR2365154A1 (enExample)
GB (1) GB1591902A (enExample)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2469346A1 (fr) * 1979-08-22 1981-05-22 Rca Corp Dispositif de commande de position pour engin spatial utilisant le jet d'ejection des fusees de direction
FR2505288A1 (fr) * 1981-05-07 1982-11-12 Aerospatiale Procede de mise sur orbite d'un satellite artificiel et agencement de satellite pour sa mise en oeuvre
FR2583873A1 (fr) * 1985-06-20 1986-12-26 Matra Procede et dispositif d'injection de satellite sur orbite geostationnaire avec stabilisation suivant les trois axes
EP0394897A1 (fr) * 1989-04-24 1990-10-31 Alcatel Espace Procédé de mise à poste d'un satellite de télécommunications géostationnaire
FR2661889A1 (fr) * 1990-05-09 1991-11-15 Europ Agence Spatiale Systeme propulsif pour un engin spatial stabilise en rotation et procede de commande de sa mise a feu.
US5251855A (en) * 1990-05-09 1993-10-12 Agence Spatiale Europeenne Spacecraft propulsion system thruster firing system
FR3006670A1 (fr) * 2013-06-07 2014-12-12 Thales Sa Systeme de propulsion en deux modules pour controle d'orbite et controle d'attitude de satellite

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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
DE3214374C2 (de) * 1982-04-20 1986-01-16 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zum Einstellen der Umlaufbahn eines dreiachsenstabilisierten Erdsatelliten
US4618112A (en) * 1983-04-15 1986-10-21 Rca Corporation Spacecraft angular momentum stabilization system and method
US4591118A (en) * 1984-02-17 1986-05-27 Ford Aerospace & Communications Corporation Hysteresis conditioner for spacecraft attitude control
US4609169A (en) * 1984-08-14 1986-09-02 The United States Of America As Represented By The Secretary Of The Air Force Propellant tank resupply system
US4630790A (en) * 1984-11-19 1986-12-23 Ford Aerospace & Communications Corporation Velocity and attitude control for exoatmospheric projectile
FR2580582B1 (fr) * 1985-04-19 1987-06-26 Matra Procede et dispositif d'amortissement de nutation de satellite par commande d'orientation de masses presentant un produit d'inertie variable
US4837699A (en) * 1985-07-18 1989-06-06 Hughes Aircraft Company Method for controlling the spin axis attitude of a spinning spacecraft
DE3674374D1 (de) 1985-07-18 1990-10-25 Hughes Aircraft Co Selbstaendige lageaenderung der spinachse eines drallstabilisierten raumfahrzeuges.
US4776541A (en) * 1985-09-24 1988-10-11 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Fluidic momentum controller
US4711414A (en) * 1986-03-31 1987-12-08 The Boeing Company Projectile with integrated propulsion system
GB8610849D0 (en) * 1986-05-02 1986-08-20 Marconi Co Ltd Gas thruster
US4767084A (en) * 1986-09-18 1988-08-30 Ford Aerospace & Communications Corporation Autonomous stationkeeping for three-axis stabilized spacecraft
US4911385A (en) * 1987-04-30 1990-03-27 Agrawal Brij N Attitude pointing error correction system and method for geosynchronous satellites
US4768350A (en) * 1987-06-15 1988-09-06 Moran Jr Henry A/C - evaporative cooler sun shroud
DE3885883D1 (de) * 1987-09-16 1994-01-05 Deutsche Aerospace Vorrichtung zur sollwertregelung und/oder stabilisierung von freibeweglichen körpern mit gespeichertem drall.
US4848706A (en) * 1988-02-29 1989-07-18 Ford Aerospace Corporation Spacecraft attitude control using coupled thrusters
US4916622A (en) * 1988-06-16 1990-04-10 General Electric Company Attitude control system
FR2637565B1 (fr) * 1988-10-06 1991-01-11 Aerospatiale Systeme de controle actif selon trois axes de l'attitude d'un satellite geostationnaire
JPH0825519B2 (ja) * 1988-10-25 1996-03-13 日本電気株式会社 人工衛星の軌道制御装置
US5012992A (en) * 1988-12-09 1991-05-07 Hughes Aircraft Company Spin stabilization via momentum wheels or similar devices
US4997146A (en) * 1989-05-30 1991-03-05 Ford Aerospace Corporation Electronic sun incidence avoidance device
FR2650135B1 (fr) * 1989-07-19 1994-05-20 Centre Nal Etudes Spatiales Satellite et procede de mise en orbite par assistance gravitationnelle
US5169094A (en) * 1990-02-26 1992-12-08 Aerospatiale Societe Nationale Industrielle Geostationary earth observation satellite incorporating liquid propellant apogee maneuver system and hollow antennas
US5172876A (en) * 1990-08-03 1992-12-22 Space Systems/Loral, Inc. Spin reorientation maneuver for spinning spacecraft
WO1992003339A1 (en) * 1990-08-22 1992-03-05 Microcosm, Inc. Satellite orbit maintenance system
FR2669887B1 (fr) * 1990-11-30 1995-06-02 Aerospatiale Procede de controle d'attitude en tangage d'un satellite grace a la pression de radiation solaire et satellite adapte a sa mise en óoeuvre.
US5222023A (en) * 1991-04-02 1993-06-22 Space Systems/Loral, Inc. Compensated transition for spacecraft attitude control
DE4129630A1 (de) * 1991-09-06 1993-05-06 Deutsche Aerospace Ag, 8000 Muenchen, De Messanordnung und regelungssystem zur lageregelung eines dreiachsenstabilisierten satelliten sowie zugehoerige mess- und regelverfahren
DE4129628A1 (de) * 1991-09-06 1993-03-18 Deutsche Aerospace Verfahren und vorrichtung zur lageregelung eines dreiachsenstabilisierten, drallbehafteten raumfahrzeuges
US5687084A (en) * 1992-05-26 1997-11-11 Microcosm, Inc. Satellite orbit maintenance system
US20030236070A1 (en) 2002-06-25 2003-12-25 Seligsohn Sherwin I. Sub-orbital, high altitude communications system
EP0711476B1 (en) 1993-07-30 1999-10-13 International Multi-Media Corporation Sub-orbital, high altitude communications system
US5459669A (en) * 1994-02-14 1995-10-17 Space Systems/Loral, Inc. Control system and method for spacecraft attitude control
US5850993A (en) * 1995-08-25 1998-12-22 Martin Marietta Corp. Spacecraft thruster operation for improved orbital maneuver accuracy
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
US5992799A (en) * 1996-03-08 1999-11-30 Space Systems/Loral, Inc. Earth based spacecraft orbit and attitude control using a look-ahead thruster selection logic and magnetic torquers
FR2757824B1 (fr) * 1996-12-31 1999-03-26 Europ Propulsion Procede et systeme de lancement de satellites sur des orbites non coplanaires en utilisant l'assistance gravitationnelle lunaire
WO1998032657A1 (en) * 1997-01-27 1998-07-30 Space Systems/Loral, Inc. Spacecraft attitude control system using low thrust thrusters
US6053455A (en) * 1997-01-27 2000-04-25 Space Systems/Loral, Inc. Spacecraft attitude control system using low thrust thrusters
AU6649798A (en) 1997-02-04 1998-08-25 Edward A. Belbruno New procedure for generating operational ballistic capture transfer using a computer implemented process
WO1998042570A2 (en) * 1997-03-25 1998-10-01 Belbruno Edward A Method for changing inclinations of orbiting satellites
US6097997A (en) * 1997-03-25 2000-08-01 Galaxy Development, Llc Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same
EA002665B1 (ru) 1997-04-24 2002-08-29 Галакси Девелопмент, Ллс Способ изменения наклонения и высоты орбиты космического летательного аппарата с использованием границ области малой устойчивости
KR100221559B1 (ko) * 1997-05-15 1999-09-15 정선종 위성의 온보드 자동 제어 방법
US7198230B2 (en) * 1997-10-14 2007-04-03 The Directv Group, Inc. Method and system for maximizing satellite constellation coverage
US6032903A (en) * 1998-02-12 2000-03-07 Hughes Electronics Corporation Cooperative control structures and methods for satellite spin axis control
US6193193B1 (en) * 1998-04-01 2001-02-27 Trw Inc. Evolvable propulsion module
US6296207B1 (en) * 1999-01-27 2001-10-02 Space Systems/Loral, Inc. Combined stationkeeping and momentum management
RU2149805C1 (ru) * 1999-02-09 2000-05-27 Опытное конструкторское бюро "Факел" Реактивная система управления движением космического аппарата
US6385512B1 (en) 1999-04-16 2002-05-07 Galaxy Development Llc System and method of a ballistic capture transfer to L4, L5
ES2180367B1 (es) * 2000-03-01 2004-04-01 Centro De Investigacion De Tecnicas Aeroespaciales, S.A. (Cenita) Nuevo procedimiento para modificar la trayectoria de un cuerpo movil o particula.
ES2171355B1 (es) * 2000-10-10 2003-12-01 Cenita S A Un sistema y un metodo para modificar y controlar trayectorias de ingenios en navegacion espacial o aerea, y para modificar trayectorias de cuerpos inertes que se desplazan por el espacio.
US7090171B2 (en) 2003-01-14 2006-08-15 Honeywell International, Inc. Momentum stabilized launch vehicle upper stage
US7832687B1 (en) 2004-08-24 2010-11-16 Lockheed Martin Corporation On-orbit storage, plane change, and injection to final orbit of space vehicles
US8319162B2 (en) * 2008-12-08 2012-11-27 Raytheon Company Steerable spin-stabilized projectile and method
CN101758933B (zh) * 2009-12-30 2012-08-22 北京控制工程研究所 基于发动机前后配置的姿轨控制方法
US9342108B2 (en) 2011-09-16 2016-05-17 Apple Inc. Protecting an electronic device
US9432492B2 (en) 2013-03-11 2016-08-30 Apple Inc. Drop countermeasures for electronic device
US9505032B2 (en) 2013-03-14 2016-11-29 Apple Inc. Dynamic mass reconfiguration
US20150001344A1 (en) * 2013-06-26 2015-01-01 Raytheon Company Satellite positioning system
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US10005568B2 (en) * 2015-11-13 2018-06-26 The Boeing Company Energy efficient satellite maneuvering
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CN113031638B (zh) * 2021-03-10 2022-08-23 哈尔滨工业大学 基于小推力卫星分时调相的星座部署方法、装置及存储介质
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FR2259389A1 (enExample) * 1974-01-25 1975-08-22 Hughes Aircraft Co

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FR2259389A1 (enExample) * 1974-01-25 1975-08-22 Hughes Aircraft Co

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2469346A1 (fr) * 1979-08-22 1981-05-22 Rca Corp Dispositif de commande de position pour engin spatial utilisant le jet d'ejection des fusees de direction
FR2505288A1 (fr) * 1981-05-07 1982-11-12 Aerospatiale Procede de mise sur orbite d'un satellite artificiel et agencement de satellite pour sa mise en oeuvre
EP0064917A1 (fr) * 1981-05-07 1982-11-17 AEROSPATIALE Société Nationale Industrielle Procédé de mise sur orbite d'un satellite artificiel
FR2583873A1 (fr) * 1985-06-20 1986-12-26 Matra Procede et dispositif d'injection de satellite sur orbite geostationnaire avec stabilisation suivant les trois axes
EP0209429A1 (fr) * 1985-06-20 1987-01-21 Matra Procédé et dispositif d'injection de satellite sur orbite géostationnaire avec stabilisation suivant les trois axes
EP0394897A1 (fr) * 1989-04-24 1990-10-31 Alcatel Espace Procédé de mise à poste d'un satellite de télécommunications géostationnaire
FR2647565A1 (fr) * 1989-04-24 1990-11-30 Alcatel Espace Procede de mise a poste d'un satellite de telecommunications geostationnaire
FR2661889A1 (fr) * 1990-05-09 1991-11-15 Europ Agence Spatiale Systeme propulsif pour un engin spatial stabilise en rotation et procede de commande de sa mise a feu.
US5251855A (en) * 1990-05-09 1993-10-12 Agence Spatiale Europeenne Spacecraft propulsion system thruster firing system
FR3006670A1 (fr) * 2013-06-07 2014-12-12 Thales Sa Systeme de propulsion en deux modules pour controle d'orbite et controle d'attitude de satellite
EP2810875A3 (fr) * 2013-06-07 2015-05-20 Thales Système de propulsion en deux modules pour contrôle d'orbite et contrôle d'attitude de satellite
US9957067B2 (en) 2013-06-07 2018-05-01 Thales Propulsion system in two modules for satellite orbit control and attitude control

Also Published As

Publication number Publication date
GB1591902A (en) 1981-07-01
DE2642061A1 (de) 1978-03-23
FR2365154B1 (enExample) 1981-05-08
DE2642061C2 (de) 1983-11-24
US4288051A (en) 1981-09-08

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