DE2642061A1 - Lageregelungs- und bahnaenderungsverfahren fuer einen dreiachsenstabilisierbaren satelliten, insbesondere fuer einen geostationaeren satelliten und einrichtung zur durchfuehrung des verfahrens - Google Patents

Lageregelungs- und bahnaenderungsverfahren fuer einen dreiachsenstabilisierbaren satelliten, insbesondere fuer einen geostationaeren satelliten und einrichtung zur durchfuehrung des verfahrens

Info

Publication number
DE2642061A1
DE2642061A1 DE19762642061 DE2642061A DE2642061A1 DE 2642061 A1 DE2642061 A1 DE 2642061A1 DE 19762642061 DE19762642061 DE 19762642061 DE 2642061 A DE2642061 A DE 2642061A DE 2642061 A1 DE2642061 A1 DE 2642061A1
Authority
DE
Germany
Prior art keywords
satellite
bahnaenderungsverfahren
dreiachsenstabilisierbaren
control
geostationary
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
DE19762642061
Other languages
English (en)
Other versions
DE2642061C2 (de
Inventor
Wilhelm Dipl Phys Goeschel
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
Priority to DE2642061A priority Critical patent/DE2642061C2/de
Publication of DE2642061A1 publication Critical patent/DE2642061A1/de
Application granted granted Critical
Publication of DE2642061C2 publication Critical patent/DE2642061C2/de
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/285Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum wheels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244Attitude control
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26Guiding or controlling apparatus, e.g. for attitude control using jets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/281Spin-stabilised spacecraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/283Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
DE2642061A 1976-09-18 1976-09-18 Expired DE2642061C2 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE2642061A DE2642061C2 (de) 1976-09-18 1976-09-18

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE2642061A DE2642061C2 (de) 1976-09-18 1976-09-18
GB37207/77A GB1591902A (en) 1976-09-18 1977-09-06 Method for controlling the attitude and orbital path of a satellite
FR7727476A FR2365154B1 (de) 1976-09-18 1977-09-12
US06/031,526 US4288051A (en) 1976-09-18 1979-04-19 Method and apparatus for controlling a satellite

Publications (2)

Publication Number Publication Date
DE2642061A1 true DE2642061A1 (de) 1978-03-23
DE2642061C2 DE2642061C2 (de) 1983-11-24

Family

ID=5988259

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2642061A Expired DE2642061C2 (de) 1976-09-18 1976-09-18

Country Status (4)

Country Link
US (1) US4288051A (de)
DE (1) DE2642061C2 (de)
FR (1) FR2365154B1 (de)
GB (1) GB1591902A (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3214374A1 (de) * 1982-04-20 1983-10-27 Mitsubishi Electric Corp Verfahren zum einstellen der umlaufbahn eines dreiachsenstabilisierten satelliten
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

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FR2505288B1 (de) * 1981-05-07 1983-07-22 Aerospatiale
US4618112A (en) * 1983-04-15 1986-10-21 Rca Corporation Spacecraft angular momentum stabilization system and method
WO1985003686A1 (en) * 1984-02-17 1985-08-29 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
FR2583873B1 (fr) * 1985-06-20 1987-09-11 Matra Procede et dispositif d'injection de satellite sur orbite geostationnaire avec stabilisation suivant les trois axes
EP0231273B1 (de) 1985-07-18 1990-09-19 Hughes Aircraft Company Selbständige lageänderung der spinachse eines drallstabilisierten raumfahrzeuges
US4837699A (en) * 1985-07-18 1989-06-06 Hughes Aircraft Company Method for controlling the spin axis attitude of a spinning spacecraft
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
EP0333808B1 (de) * 1987-09-16 1993-11-24 Deutsche Aerospace AG 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
FR2647565B1 (fr) * 1989-04-24 1991-07-26 Alcatel Espace Procede de mise a poste d'un satellite de telecommunications geostationnaire
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
US5251855A (en) * 1990-05-09 1993-10-12 Agence Spatiale Europeenne Spacecraft propulsion system thruster firing system
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.
US5172876A (en) * 1990-08-03 1992-12-22 Space Systems/Loral, Inc. Spin reorientation maneuver for spinning spacecraft
US5687084A (en) * 1992-05-26 1997-11-11 Microcosm, Inc. Satellite orbit maintenance system
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
DE4129628A1 (de) * 1991-09-06 1993-03-18 Deutsche Aerospace Verfahren und vorrichtung zur lageregelung eines dreiachsenstabilisierten, drallbehafteten raumfahrzeuges
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
DE4495639T1 (de) 1993-07-30 1996-10-31 Int Multi Media Co Suborbitales Kommunikationssystem mit größer Höhe
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
US6053455A (en) * 1997-01-27 2000-04-25 Space Systems/Loral, Inc. Spacecraft attitude control system using low thrust thrusters
WO1998032657A1 (en) * 1997-01-27 1998-07-30 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
AU738202B2 (en) 1997-04-24 2001-09-13 Galaxy Development, Llc. Satellite inclination changes using weak stability boundaries
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
AU7357198A (en) 1997-03-25 1998-10-20 Edward A. Belbruno Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same
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
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.
US20030236070A1 (en) 2002-06-25 2003-12-25 Seligsohn Sherwin I. Sub-orbital, high altitude communications system
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
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
FR3006670B1 (fr) * 2013-06-07 2015-05-29 Thales Sa Systeme de propulsion en deux modules pour controle d'orbite et controle d'attitude de satellite
US20150001344A1 (en) * 2013-06-26 2015-01-01 Raytheon Company Satellite positioning system
US9715257B2 (en) 2014-04-18 2017-07-25 Apple Inc. Active screen protection for electronic device
KR101688331B1 (ko) * 2015-09-10 2016-12-20 한국항공우주연구원 위성체 제어 장치 및 그 방법
US10005568B2 (en) * 2015-11-13 2018-06-26 The Boeing Company Energy efficient satellite maneuvering

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US3866025A (en) * 1972-03-17 1975-02-11 Rca Corp Spacecraft attitude control system
US3907226A (en) * 1970-07-06 1975-09-23 Hughes Aircraft Co Redundant position and attitude control for spin stabilized devices

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US3231223A (en) * 1962-11-16 1966-01-25 Thiokol Chemical Corp Flight attitude control system
US3511452A (en) * 1967-02-24 1970-05-12 Trw Inc Spinning body attitude control
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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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3214374A1 (de) * 1982-04-20 1983-10-27 Mitsubishi Electric Corp Verfahren zum einstellen der umlaufbahn eines dreiachsenstabilisierten satelliten
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

Also Published As

Publication number Publication date
DE2642061C2 (de) 1983-11-24
GB1591902A (en) 1981-07-01
FR2365154A1 (fr) 1978-04-14
FR2365154B1 (de) 1981-05-08
US4288051A (en) 1981-09-08

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Legal Events

Date Code Title Description
OD Request for examination
8181 Inventor (new situation)

Free format text: GOESCHEL, WILHELM, DIPL.-PHYS., 8021 TAUFKIRCHEN, DE

D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee