DE69111437D1 - Verfahren zur steuerung des nickwinkels eines satelliten mittels sonnenwinddruck und satellit zur durchführung desselben. - Google Patents

Verfahren zur steuerung des nickwinkels eines satelliten mittels sonnenwinddruck und satellit zur durchführung desselben.

Info

Publication number
DE69111437D1
DE69111437D1 DE69111437T DE69111437T DE69111437D1 DE 69111437 D1 DE69111437 D1 DE 69111437D1 DE 69111437 T DE69111437 T DE 69111437T DE 69111437 T DE69111437 T DE 69111437T DE 69111437 D1 DE69111437 D1 DE 69111437D1
Authority
DE
Germany
Prior art keywords
satellite
nickle
implementing
controlling
angle
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
DE69111437T
Other languages
English (en)
Other versions
DE69111437T2 (de
Inventor
Patrick Flament
Michel Perdu
Jean Portier
Pierre Brunet
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 DE69111437D1 publication Critical patent/DE69111437D1/de
Application granted granted Critical
Publication of DE69111437T2 publication Critical patent/DE69111437T2/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
    • B64G1/40—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
    • B64G1/244—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
    • B64G1/24—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
    • 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
    • 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
    • B64G1/34—Guiding or controlling apparatus, e.g. for attitude control using gravity gradient
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • 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
    • B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Automation & Control Theory (AREA)
  • Environmental & Geological Engineering (AREA)
  • Geology (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Sustainable Energy (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE69111437T 1990-11-30 1991-11-26 Verfahren zur steuerung des nickwinkels eines satelliten mittels sonnenwinddruck und satellit zur durchführung desselben. Expired - Fee Related DE69111437T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9015050A FR2669887B1 (fr) 1990-11-30 1990-11-30 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.
PCT/FR1991/000938 WO1992009479A2 (fr) 1990-11-30 1991-11-26 Procede de controle d'attitude en tangage d'un satellite grace a la pression de radiation solaire et satellite adapte a sa mise en ×uvre

Publications (2)

Publication Number Publication Date
DE69111437D1 true DE69111437D1 (de) 1995-08-24
DE69111437T2 DE69111437T2 (de) 1996-01-04

Family

ID=9402801

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69111437T Expired - Fee Related DE69111437T2 (de) 1990-11-30 1991-11-26 Verfahren zur steuerung des nickwinkels eines satelliten mittels sonnenwinddruck und satellit zur durchführung desselben.

Country Status (8)

Country Link
US (3) US5312073A (de)
EP (1) EP0519038B1 (de)
JP (1) JP3220142B2 (de)
CA (1) CA2074959A1 (de)
DE (1) DE69111437T2 (de)
FR (1) FR2669887B1 (de)
RU (1) RU2114770C1 (de)
WO (1) WO1992009479A2 (de)

Families Citing this family (77)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4114804A1 (de) * 1991-05-07 1992-11-12 Messerschmitt Boelkow Blohm Vorrichtung zur lageregelung von satelliten mit solardruckmomenten
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
US5310144A (en) * 1992-07-06 1994-05-10 Hughes Aircraft Company Method and apparatus for satellite torque balancing
US6021979A (en) * 1993-07-19 2000-02-08 Hughes Electronics Corporation Sun-referenced safe-hold control for momentum biased satellites
US6365334B1 (en) 1993-10-22 2002-04-02 Eastman Kodak Company Photographic elements containing aryloxypyrazolone couplers and sulfur containing stabilizers
EP0692425A1 (de) * 1994-07-14 1996-01-17 Orbital Sciences Corporation Verfahren und System zur Positionshaltung zwischen im Orbit befindlichen Raumflugkörpern durch Änderung ihrer ballistischen Koeffizienten
US5669586A (en) * 1994-12-06 1997-09-23 Space Systems/Loral, Inc. Satellite gravity gradient compensation using on-orbit solar array reorientation
US5618012A (en) * 1995-01-12 1997-04-08 Space Systems/Loral, Inc. Satellite stabilization system
US5833175A (en) * 1995-12-22 1998-11-10 Hughes Electronics Corporation Spacecraft with large east-west dimensions
US5984236A (en) * 1995-12-22 1999-11-16 Keitel; Keith F. Momentum unloading using gimbaled thrusters
US5819526A (en) * 1996-02-23 1998-10-13 Trw Inc. Low power arcjet propellant feed system
US5934620A (en) * 1996-03-04 1999-08-10 Abernethy; David K. Spacecraft sun-target steering about an arbitrary body axis
US5895014A (en) * 1996-07-31 1999-04-20 Hughes Electronics Corporation Satellite solar array and method of biasing to reduce seasonal output power fluctuations
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
US6053455A (en) * 1997-01-27 2000-04-25 Space Systems/Loral, Inc. Spacecraft attitude control system using low thrust thrusters
US5850197A (en) * 1997-08-25 1998-12-15 Trimble Navigation Attitude determination using fewer than three antennas
US6029438A (en) * 1997-10-15 2000-02-29 Space Systems/Loral, Inc. Drive circuit for electric propulsion thruster
US6032904A (en) * 1998-02-23 2000-03-07 Space Systems/Loral, Inc. Multiple usage thruster mounting configuration
DE19907235A1 (de) * 1999-02-19 2000-09-14 Daimler Chrysler Ag GPS-Navigationssystem für Raumfahrtanwendungen
US6373023B1 (en) 1999-03-02 2002-04-16 General Dynamics (Ots) Aerospace, Inc. ARC discharge initiation for a pulsed plasma thruster
US6550720B2 (en) * 1999-07-09 2003-04-22 Aeroastro Aerobraking orbit transfer vehicle
US6675324B2 (en) * 1999-09-27 2004-01-06 Intel Corporation Rendezvous of processors with OS coordination
US6194790B1 (en) * 1999-11-22 2001-02-27 The United States Of America As Represented By The Secretary Of The Air Force Solar sail for power generation
US6481671B1 (en) * 2000-08-14 2002-11-19 Ball Aerospace & Technologies Corp. Spacecraft sunshield for use in performing solar torque balancing
FR2821683B1 (fr) * 2001-03-01 2003-06-13 Agence Spatiale Europeenne Procede de commande pour controler ou stabiliser l'orientation d'un engin dans l'espace
JP3859454B2 (ja) * 2001-03-01 2006-12-20 Ｎｅｃ東芝スペースシステム株式会社 人工衛星のマヌーバ制御装置
US6581880B2 (en) * 2001-10-15 2003-06-24 Space Systems/Loral, Inc. Energy managed electric propulsion methods and systems for stationkeeping satellites
GB0203950D0 (en) * 2002-02-20 2002-04-03 Astrium Ltd Method and system for balancing thrust demands
US6990396B2 (en) * 2002-12-13 2006-01-24 The Boeing Company Method and apparatus for reaction wheel dynamic compensation in long-duration deployment of a large reflector
US7025307B2 (en) * 2002-12-13 2006-04-11 The Boeing Company Method and apparatus for solar tacking momentum maintenance in long-duration deployment of a large reflector
US6921050B2 (en) * 2003-01-17 2005-07-26 Northrop Grumman Corporation Solar torque control using thin film directionally reflective, emissive, absorptive and transmissive surfaces
US20050077425A1 (en) * 2003-10-10 2005-04-14 Raymond Payette Thruster for propelling and directing a vehicle without interacting with environment and method for making the same
US20050211828A1 (en) * 2004-03-09 2005-09-29 Aeroastro, Inc. Aerodynamic orbit inclination control
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
GB2460443A (en) * 2008-05-29 2009-12-02 Inmarsat Global Ltd Propulsion system arrangement for decommissioning a satellite
AT507213B1 (de) * 2008-09-03 2010-03-15 Austrian Aerospace Gmbh Antriebseinrichtung zum verstellen von zu orientierenden bauteilen eines raumfahrzeugs
FR2937954B1 (fr) 2008-10-31 2011-07-29 Thales Sa Procede et systeme de desaturation des roues d'inertie d'un engin spatial
US8186628B2 (en) * 2009-08-12 2012-05-29 Raytheon Company Multi-axis articulated solar light shade for space-based sensors
CN102081156B (zh) * 2009-11-30 2013-12-18 上海卫星工程研究所 合成孔径雷达卫星的驱动机构
US8561944B2 (en) 2010-06-17 2013-10-22 Lockheed Martin Corporation System and method for desaturation of a control moment gyroscope
US20120181386A1 (en) * 2011-01-13 2012-07-19 Vaclav Majer Eccentricity vector control with continuous or quasi-continuous maneuvers
US8735788B2 (en) * 2011-02-18 2014-05-27 Raytheon Company Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control
FR2980176A1 (fr) * 2011-09-19 2013-03-22 Astrium Sas Procede de controle d'attitude d'un satellite et satellite commande en attitude
FR2986213B1 (fr) * 2012-02-01 2014-10-10 Snecma Engin spatial a propulsion electrique et chimique a propergol solide
US20130327015A1 (en) * 2012-06-12 2013-12-12 Pamela Pollet Dual use hydrazine propulsion thruster system
FR3013685B1 (fr) * 2013-11-25 2017-05-19 Astrium Sas Procede et dispositif de commande d'une phase d'acquisition du soleil par un engin spatial
FR3014082B1 (fr) * 2013-11-29 2016-01-01 Thales Sa Systeme de tuyeres et procede pour le controle d'orbite et d'attitude pour satellite geostationnaire
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
US9087451B1 (en) 2014-07-14 2015-07-21 John A. Jarrell Unmanned aerial vehicle communication, monitoring, and traffic management
US9764858B2 (en) * 2015-01-07 2017-09-19 Mitsubishi Electric Research Laboratories, Inc. Model predictive control of spacecraft
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
CN104714554B (zh) * 2015-03-17 2017-07-28 北京航空航天大学 一种共位式卫星编队的构造方法
CN104787360B (zh) * 2015-03-18 2017-01-04 北京空间飞行器总体设计部 一种基于轨迹保持需求的遥感卫星空间碎片规避机动方法
CN105183948B (zh) * 2015-08-13 2018-04-10 北京空间飞行器总体设计部 一种基于二次反射的高精度卫星太阳光压摄动力建模方法
US9522746B1 (en) * 2015-08-27 2016-12-20 The Boeing Company Attitude slew methodology for space vehicles using gimbaled low-thrust propulsion subsystem
US10618678B1 (en) * 2015-10-20 2020-04-14 Space Systems/Loral, Llc Self-balancing solar array
RU2614467C1 (ru) * 2015-10-27 2017-03-28 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ формирования управляющих воздействий на космический аппарат с силовыми гироскопами и поворотными солнечными батареями
US10005568B2 (en) * 2015-11-13 2018-06-26 The Boeing Company Energy efficient satellite maneuvering
US10647450B2 (en) * 2016-03-18 2020-05-12 The Boeing Company Satellite control system using electrically controllable variable reflection glass panels
US10529221B2 (en) 2016-04-19 2020-01-07 Navio International, Inc. Modular approach for smart and customizable security solutions and other applications for a smart city
US10435184B2 (en) 2016-05-06 2019-10-08 Darrin Taylor Method of space travel using a high acceleration thrust vehicle in combination with a plurality of low acceleration thrust vehicles
FR3052269B1 (fr) * 2016-06-03 2018-07-06 Thales Procede de controle d'attitude d' un engin spatial, produit programme d'ordinateur et module de controle associes
US11338942B2 (en) * 2016-06-14 2022-05-24 Richard Stuart Blomquist Spacecraft and control method
CN106096148B (zh) * 2016-06-14 2019-05-24 中国空间技术研究院 一种简单姿态控制下的大倾角轨道卫星太阳帆板指向方法
KR101898641B1 (ko) * 2017-08-16 2018-10-31 한국항공우주연구원 인공위성 및 이의 제어 방법
KR102018193B1 (ko) * 2018-05-08 2019-09-04 한국항공우주연구원 인공위성 및 이의 자세 제어 방법
US10954004B2 (en) * 2018-07-17 2021-03-23 The Aerospace Corporation Energy extraction and storage, and propulsion systems for space vehicles
WO2020206096A1 (en) * 2019-04-03 2020-10-08 Xplore Inc. Spacecraft mass shifting with propellant tank systems
EP3983297A4 (de) * 2019-06-17 2023-06-21 The Board Of Trustees Of The University Of Illinois Multifunktionsstrukturen zur lageregelung
RU2726152C1 (ru) * 2019-12-09 2020-07-09 Федеральное государственное бюджетное военное образовательное учреждение высшего образования "Военно-космическая академия имени А.Ф. Можайского" Министерства обороны Российской Федерации Электрический ракетный двигатель (варианты)
CN112016187B (zh) * 2020-07-27 2022-08-09 中国空气动力研究与发展中心计算空气动力研究所 一种基于混合动力的近地小行星交会任务轨道优化方法
CN114987802A (zh) * 2020-12-08 2022-09-02 中国科学院微小卫星创新研究院 基于运动部件信息的角动量前馈补偿控制方法
US11926442B2 (en) 2021-04-07 2024-03-12 Ball Aerospace & Technologies Corp. Multiple function spacecraft sunshade systems and methods
CN115892507A (zh) * 2023-01-09 2023-04-04 中国科学院微小卫星创新研究院 卫星、卫星模块组件及卫星模块连接单元

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2604005A1 (de) * 1976-02-03 1977-08-11 Messerschmitt Boelkow Blohm Einrichtung zur beeinflussung der position und lage eines satelliten
DE2642061C2 (de) * 1976-09-18 1983-11-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Lageregelungs- und Bahnänderungsverfahren für einen dreiachsenstabilisierbaren Satelliten, insbesondere für einen geostationären Satelliten und Einrichtung zur Durchführung des Verfahrens
FR2522614A1 (fr) * 1982-03-02 1983-09-09 Centre Nat Etd Spatiales Configuration de satellite a orbite equatoriale a moyens solaires perfectionnes
US4759517A (en) * 1982-06-25 1988-07-26 General Electric Company Station-keeping using solar sailing
DE3329955A1 (de) * 1983-08-19 1985-03-07 Erno Raumfahrttechnik Gmbh, 2800 Bremen Lageregelung von satelliten
US4684084A (en) * 1984-05-29 1987-08-04 Rca Corporation Spacecraft structure with symmetrical mass center and asymmetrical deployable appendages
US4630790A (en) * 1984-11-19 1986-12-23 Ford Aerospace & Communications Corporation Velocity and attitude control for exoatmospheric projectile
US4728061A (en) * 1985-03-20 1988-03-01 Space Industries, Inc. Spacecraft operable in two alternative flight modes
US4747567A (en) * 1985-03-20 1988-05-31 Space Industries, Inc. Spacecraft with articulated solar array
US4767084A (en) * 1986-09-18 1988-08-30 Ford Aerospace & Communications Corporation Autonomous stationkeeping for three-axis stabilized spacecraft
US4825646A (en) * 1987-04-23 1989-05-02 Hughes Aircraft Company Spacecraft with modulated thrust electrostatic ion thruster and associated method
FR2615477B1 (fr) * 1987-05-22 1989-08-18 Centre Nat Etd Spatiales Dispositif et procede de pointage d'une sonde spatiale vers un corps celeste
JPH01237296A (ja) * 1988-03-18 1989-09-21 Mitsubishi Electric Corp 太陽電地パドル装置
JP2685225B2 (ja) * 1988-05-26 1997-12-03 宇宙開発事業団 人工衛星の姿勢制御装置
US4949922A (en) * 1988-12-09 1990-08-21 Hughes Aircraft Company Satellite control system
US5020746A (en) * 1989-09-29 1991-06-04 Hughes Aircraft Company Method for satellite station keeping
FR2655167B1 (fr) * 1989-11-29 1992-04-03 Aerospatiale Procede de controle d'attitude en roulis et en lacet d'un satellite.
US5310144A (en) * 1992-07-06 1994-05-10 Hughes Aircraft Company Method and apparatus for satellite torque balancing

Also Published As

Publication number Publication date
FR2669887B1 (fr) 1995-06-02
RU2114770C1 (ru) 1998-07-10
US5312073A (en) 1994-05-17
DE69111437T2 (de) 1996-01-04
WO1992009479A2 (fr) 1992-06-11
EP0519038A1 (de) 1992-12-23
JPH05504118A (ja) 1993-07-01
CA2074959A1 (en) 1992-05-31
US5850992A (en) 1998-12-22
JP3220142B2 (ja) 2001-10-22
EP0519038B1 (de) 1995-07-19
FR2669887A1 (fr) 1992-06-05
WO1992009479A3 (fr) 1992-11-26
US5626315A (en) 1997-05-06

Similar Documents

Publication Publication Date Title
DE69111437T2 (de) Verfahren zur steuerung des nickwinkels eines satelliten mittels sonnenwinddruck und satellit zur durchführung desselben.
DE69411298D1 (de) Verfahren zur Steuerung eines Kraftwerks und Kraftwerk
DE59004038D1 (de) Verfahren und Anordnung zur Steuerung eines Scheibenwischers.
DE69126233D1 (de) Vorrichtung zur Steuerung der Lage eines Satelliten in einer geneigten Umlaufbahn
DE69423955D1 (de) System zur Erfassung der Position eines beweglichen Roboters und dessen Steuerungsverfahren
DE69217844D1 (de) Verfahren und Gerät zur Steuerung eines Satellitensonnenkollektors mittels eines Sonnensensors
DE69634768D1 (de) Vorrichtung zur Steuerung der Position eines Trägertisches, sowie Trägertischvorrichtung, Belichtungsgerät und Herstellungsverfahren unter Verwendung derselben
DE69016246D1 (de) Verfahren und Gerät zur Steuerung eines Plattengerätes.
DE69123947D1 (de) Verfahren zur Steuerung der Geschwindigkeit eines Fahrzeugs
DE69632570D1 (de) Wasserabsorbierendes pulver und verfahren zur herstellung
DE59305537D1 (de) Sonnenblende für Fahrzeuge sowie Verfahren und Vorrichtung zum Herstellen derselben
DE69713208D1 (de) Verfahren und System zur Steuerung des Giermomentes eines Fahrzeuges
DE69103119T2 (de) Verfahren und Vorrichtung zur Steuerung der Züchtung eines Kegelförmigen Teiles eines Einkristalles.
DE69615318D1 (de) Verfahren zur Lagesteuerung eines Satteliten mit niederer Umlaufbahn mittels Sonnenerfassung
DE69206204T2 (de) Verfahren und Vorrichtung zur kontinuierlichen und unidirektionalen Roll- und Gierlagesteuerung eines Satelliten.
DE3667645D1 (de) Verfahren und vorrichtung zur nutationsdaempfung eines satelliten durch steuerung der gewichtslagebestimmung.
DE69113917T2 (de) Verfahren und Einrichtung zur Steuerung der Bewegung eines Maschinenteiles.
DE69632033D1 (de) Verfahren und vorrichtung zur steuerung der bewegung eines virtuellen körpers
DE69625469D1 (de) Verfahren zur korrektur des ausgangsignals eines steuergerätes, steuergerät und steuergerät für hydraulikpumpe
DE69517423D1 (de) Gerät zur manuellen steuerung der bewegung eines realen oder imaginären objektes
DE69626492D1 (de) Verfahren zur steuerung des stroms eines servomotor
DE69713720D1 (de) Methode zum Schutz eines Flugzeuges vor Querwindstössen und Vorrichtung zum Steuern der Höhe eines Flugzeuges die die obengenannte Methode anwendet
DE69406097D1 (de) System zur Steuerung der Versorgung eines Asynchronmotors
DE68907942T3 (de) Verfahren zur Steuerung eines Matrixbildschirms und Vorrichtung zur Durchführung dieses Verfahrens.
DE69601853T2 (de) Verfahren und System zur Steuerung der Lage oder der Orientierung eines Raumfahrzeuges

Legal Events

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