ES2044473T3 - Sistema de control de posicion de satelite utilizando un anillo magne tico supraconductor. - Google Patents

Sistema de control de posicion de satelite utilizando un anillo magne tico supraconductor.

Info

Publication number
ES2044473T3
ES2044473T3 ES90401488T ES90401488T ES2044473T3 ES 2044473 T3 ES2044473 T3 ES 2044473T3 ES 90401488 T ES90401488 T ES 90401488T ES 90401488 T ES90401488 T ES 90401488T ES 2044473 T3 ES2044473 T3 ES 2044473T3
Authority
ES
Spain
Prior art keywords
circuit
supracductor
tico
magne
ring
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
ES90401488T
Other languages
English (en)
Inventor
Alain Reboux
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
Application granted granted Critical
Publication of ES2044473T3 publication Critical patent/ES2044473T3/es
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
    • B64G1/42—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
    • B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
    • 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
    • B64G1/285—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum wheels
    • 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)
  • Life Sciences & Earth Sciences (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Chemical & Material Sciences (AREA)
  • Geology (AREA)
  • Combustion & Propulsion (AREA)
  • Geochemistry & Mineralogy (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • Sustainable Development (AREA)
  • Photovoltaic Devices (AREA)
  • Containers, Films, And Cooling For Superconductive Devices (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Particle Accelerators (AREA)
  • Control Of Position Or Direction (AREA)

Abstract

SATELITE QUE CONSTA DE UN GENERADOR SOLAR (2) DESPLEGABLE ORIENTABLE FRENTE AL CUERPO (1) DEL SATELITE Y DESTINADO A PERMANECER SUJETO FRENTE AL SOL, ASI COMO DE UN DISPOSITIVO (4) DE ESTABILIZACION DEL COMPORTAMIENTO. SE CARACTERIZA PORQUE DICHO DISPOSITIVO DE ESTABILIZACION DEL COMPORTAMIENTO CONSTA DE AL MENOS: - UN CIRCUITO CERRADO (7) DE MATERIAL SUPRACONDUCTOR QUE VA EN UNSOPORTE ENLAZADO (6) AL GENERADOR SOLAR, Y DISPUESTO SOBRE UNA CARA DE DICHO SOPORTE QUE ESTA ORIENTADO CON OPOSICION AL SOL; - UN CIRCUITO SECUNDARIO (9) PARALELO AL CIRCUITO CERRADO, DE FORMA Y DIMENSIONES IGUALES AL CIRCUITO CERRADO, QUE VA EN DICHO SOPORTE JUNTO AL CIRCUITO; - UN CIRCUITO RESISTIVO (10) QUE VA EN DICHO SOPORTE PROXIMO A UNA PARTE DEL CIRCUITO CERRADO; Y - UN CIRCUITO ELECTRICO (11) DE ALIMENTACION SELECTIVA CONECTADO ELECTRICAMENTE AL CIRCUITO SECUNDARIO Y A CIRCUITO RESISTIVO.
ES90401488T 1989-06-23 1990-06-01 Sistema de control de posicion de satelite utilizando un anillo magne tico supraconductor. Expired - Lifetime ES2044473T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8908416A FR2648782B1 (fr) 1989-06-23 1989-06-23 Systeme de controle d'attitude de satellite utilisant une boucle magnetique supraconductrice

Publications (1)

Publication Number Publication Date
ES2044473T3 true ES2044473T3 (es) 1994-01-01

Family

ID=9383080

Family Applications (1)

Application Number Title Priority Date Filing Date
ES90401488T Expired - Lifetime ES2044473T3 (es) 1989-06-23 1990-06-01 Sistema de control de posicion de satelite utilizando un anillo magne tico supraconductor.

Country Status (7)

Country Link
US (1) US5141180A (es)
EP (1) EP0404621B1 (es)
JP (1) JP3038228B2 (es)
CA (1) CA2018386A1 (es)
DE (1) DE69003028T2 (es)
ES (1) ES2044473T3 (es)
FR (1) FR2648782B1 (es)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2682931B1 (fr) * 1991-10-28 1994-01-28 Aerospatiale Ste Nationale Indle Vehicule spatial d'observation, notamment en infrarouges, a systeme de detecteurs refroidis connectes par des fils supraconducteurs.
US5413293A (en) * 1992-12-22 1995-05-09 Hughes Aircraft Company Magnetic torque attitude control systems
US5399405A (en) * 1993-06-14 1995-03-21 Morgan Adhesives Company Trunk security seal
US6861770B2 (en) * 2001-11-13 2005-03-01 Craig Travers Using the transition state of a superconductor to produce energy
CN103818565B (zh) * 2014-03-18 2016-03-30 西北工业大学 一种pcb磁力矩器装置及其制作方法
RU2568827C1 (ru) * 2014-08-14 2015-11-20 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" (АО "ВПК "НПО машиностроения") Способ магнитной разгрузки двигателей-маховиков космического аппарата
JP6323277B2 (ja) * 2014-09-19 2018-05-16 三菱電機株式会社 太陽電池パネル
CN104570853B (zh) * 2014-12-18 2017-04-05 中国科学院长春光学精密机械与物理研究所 高可靠组合智能空间电源系统
US10618678B1 (en) * 2015-10-20 2020-04-14 Space Systems/Loral, Llc Self-balancing solar array

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH470288A (de) * 1966-02-28 1969-03-31 Gen Electric Satellit
US3390848A (en) * 1966-05-19 1968-07-02 Air Force Usa Magnetic torquing of spin axis stabilization
DE2048666A1 (de) * 1970-09-25 1972-05-31 Goeres H D Supraleitspule in Supratransformator und in Flugobjekten mit zugehörigen Kommutatoren
US4034941A (en) * 1975-12-23 1977-07-12 International Telephone And Telegraph Corporation Magnetic orientation and damping device for space vehicles
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
US4939976A (en) * 1988-04-01 1990-07-10 Minovitch Michael Andrew Electromagnetic ground to orbit propulsion method and operating system for high mass payloads
US5017549A (en) * 1989-10-31 1991-05-21 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Electromagnetic Meissner effect launcher

Also Published As

Publication number Publication date
CA2018386A1 (en) 1990-12-23
US5141180A (en) 1992-08-25
FR2648782B1 (fr) 1991-10-18
FR2648782A1 (fr) 1990-12-28
JP3038228B2 (ja) 2000-05-08
EP0404621A1 (fr) 1990-12-27
JPH0331100A (ja) 1991-02-08
DE69003028T2 (de) 1994-01-13
DE69003028D1 (de) 1993-10-07
EP0404621B1 (fr) 1993-09-01

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