FR2178668A5 - - Google Patents

Info

Publication number
FR2178668A5
FR2178668A5 FR7310994A FR7310994A FR2178668A5 FR 2178668 A5 FR2178668 A5 FR 2178668A5 FR 7310994 A FR7310994 A FR 7310994A FR 7310994 A FR7310994 A FR 7310994A FR 2178668 A5 FR2178668 A5 FR 2178668A5
Authority
FR
France
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
Application number
FR7310994A
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.)
RCA Corp
Original Assignee
RCA 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 RCA Corp filed Critical RCA Corp
Application granted granted Critical
Publication of FR2178668A5 publication Critical patent/FR2178668A5/fr
Expired 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/365—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth 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
    • B64G1/24—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
    • B64G1/285—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
    • B64G1/32—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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/366—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using magnetometers

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Environmental & Geological Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)
FR7310994A 1972-03-27 1973-03-27 Expired FR2178668A5 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00238483A US3834653A (en) 1972-03-27 1972-03-27 Closed loop roll and yaw control for satellites

Publications (1)

Publication Number Publication Date
FR2178668A5 true FR2178668A5 (fr) 1973-11-09

Family

ID=22898091

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7310994A Expired FR2178668A5 (fr) 1972-03-27 1973-03-27

Country Status (6)

Country Link
US (1) US3834653A (fr)
JP (1) JPH035360B2 (fr)
CA (1) CA990385A (fr)
DE (1) DE2315280C2 (fr)
FR (1) FR2178668A5 (fr)
GB (1) GB1424824A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2498155A1 (fr) * 1981-01-22 1982-07-23 Rca Corp Procede et appareil permettant d'amortir la nutation par application d'un couple magnetique dans la commande d'un engin spatial
FR2595147A1 (fr) * 1986-02-28 1987-09-04 Messerschmitt Boelkow Blohm Procede de determination du champ magnetique terrestre et de la position pour le controle de l'orientation d'un satellite
EP0750237A1 (fr) * 1995-06-09 1996-12-27 Daimler-Benz Aerospace Aktiengesellschaft Satellite orienté vers la terre et méthode de contrÔle de l'attitude, de la nutation et du moment d'une roue cinétique

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1544083A (en) * 1975-07-21 1979-04-11 Rca Corp Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbits
CA1073988A (fr) * 1975-07-21 1980-03-18 Ludwig Muhlfelder Commande de mouvements de roulis et en lacet a boucle fermee de precision pour satellites a orbites a faible inclinaison
US4010921A (en) * 1975-08-20 1977-03-08 The United States Of America As Represented By The Secretary Of The Air Force Spacecraft closed loop three-axis momentum unloading system
US4114841A (en) * 1977-02-22 1978-09-19 Rca Corporation Magnetic torquing system for changing the spin rate of an orbiting satellite
US4426591A (en) 1980-08-04 1984-01-17 Hughes Aircraft Company Adaptive comparator
DE3128054C2 (de) * 1981-07-16 1983-05-26 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "Einrichtung für die Roll/Gier-Regelung eines Satelliten"
US4525784A (en) * 1982-03-17 1985-06-25 Deutsche Forschungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. Steering and stabilization system for vehicles
DE3214373A1 (de) * 1982-04-20 1983-10-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren und einrichtung fuer die lageregelung eines satelliten
DE3214383A1 (de) * 1982-04-20 1983-10-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung fuer die magnetische lageregelung eines satelliten
US4591118A (en) * 1984-02-17 1986-05-27 Ford Aerospace & Communications Corporation Hysteresis conditioner for spacecraft attitude control
US4911385A (en) * 1987-04-30 1990-03-27 Agrawal Brij N Attitude pointing error correction system and method for geosynchronous satellites
US4916622A (en) * 1988-06-16 1990-04-10 General Electric Company Attitude control system
GB2241480B (en) * 1990-02-28 1993-05-26 British Aerospace Apparatus and method for controlling attitude of a spacecraft orbiting earth or other celestial body
US5123617A (en) * 1990-03-05 1992-06-23 General Electric Company Spacecraft momentum unloading using controlled magnetic torques
CA2080612A1 (fr) * 1991-11-27 1993-05-28 Douglas J. Bender Methode et dispositif pour compenser les couples de perturbation magnetique dans un satellite
US6000661A (en) * 1996-10-16 1999-12-14 Space Systems/Loral, Inc. Autonomous spacecraft payload base motion estimation and correction
US6154691A (en) * 1997-09-02 2000-11-28 Honeywell International Inc. Orienting a satellite with controlled momentum gyros
US6131056A (en) * 1998-03-16 2000-10-10 Honeywell International Inc. Continuous attitude control that avoids CMG array singularities
US6163021A (en) * 1998-12-15 2000-12-19 Rockwell Collins, Inc. Navigation system for spinning projectiles
DE19924908B4 (de) * 1999-05-31 2008-05-29 Astrium Gmbh Verfahren zur dreiachsigen Lagebestimmung für einen niedrig fliegenden Satelliten
US6592070B1 (en) * 2002-04-17 2003-07-15 Rockwell Collins, Inc. Interference-aided navigation system for rotating vehicles
US6685143B1 (en) * 2003-01-03 2004-02-03 Orbital Research Inc. Aircraft and missile forebody flow control device and method of controlling flow
US7197381B2 (en) * 2003-12-08 2007-03-27 University Of Maryland Navigational system and method utilizing sources of pulsed celestial radiation
FR2872928B1 (fr) * 2004-07-12 2006-09-15 Giat Ind Sa Procede de guidage et/ou pilotage d'un projectile et dispositif de guidage et/ou pilotage mettant en oeuvre un tel procede
EP1807676A1 (fr) * 2004-10-28 2007-07-18 University of Maryland Systeme de navigation et procede utilisant des sources de rayonnement celeste modulees
US7706932B2 (en) * 2006-11-30 2010-04-27 Instituto Nacional de Tecnica Aeroespacial “Estaban Terradas” Method for controlling control parameters in an air vehicle and system of controlling an air vehicle
DE102009024508A1 (de) * 2009-06-08 2011-07-28 Rheinmetall Air Defence Ag Verfahren zur Korrektur der Flugbahn einer endphasengelenkten Munition
US8344303B2 (en) * 2010-11-01 2013-01-01 Honeywell International Inc. Projectile 3D attitude from 3-axis magnetometer and single-axis accelerometer
CN103231810B (zh) * 2013-04-25 2015-04-22 哈尔滨工业大学 一种利用卫星俯仰轴姿态机动卸载俯仰轴角动量的方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3232561A (en) * 1963-06-06 1966-02-01 Honeywell Inc Control apparatus for space craft
US3429524A (en) * 1965-07-19 1969-02-25 Westinghouse Electric Corp Attitude control system
DE1506140A1 (de) * 1966-02-01 1969-03-27 Gen Electric Orientierungseinrichtung fuer Satelliten
US3390848A (en) * 1966-05-19 1968-07-02 Air Force Usa Magnetic torquing of spin axis stabilization
US3427453A (en) * 1966-05-25 1969-02-11 Rca Corp System for switching the attitude reference of a satellite from a first celestial body to a second celestial body
US3350548A (en) * 1966-06-17 1967-10-31 United Aircraft Corp Adaptive orbital control system for satellite navigation
US3521835A (en) * 1967-06-05 1970-07-28 Massachusetts Inst Technology Synchronous satellite
NL6914824A (fr) * 1968-10-01 1970-04-03
US3643259A (en) * 1970-02-20 1972-02-15 Ronald S Entner Navigation satellite system employing time synchronization
US3695554A (en) * 1970-10-16 1972-10-03 Rca Corp Nutation damping in dual-spin spacecraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2498155A1 (fr) * 1981-01-22 1982-07-23 Rca Corp Procede et appareil permettant d'amortir la nutation par application d'un couple magnetique dans la commande d'un engin spatial
FR2595147A1 (fr) * 1986-02-28 1987-09-04 Messerschmitt Boelkow Blohm Procede de determination du champ magnetique terrestre et de la position pour le controle de l'orientation d'un satellite
EP0750237A1 (fr) * 1995-06-09 1996-12-27 Daimler-Benz Aerospace Aktiengesellschaft Satellite orienté vers la terre et méthode de contrÔle de l'attitude, de la nutation et du moment d'une roue cinétique

Also Published As

Publication number Publication date
CA990385A (en) 1976-06-01
JPH035360B2 (fr) 1991-01-25
GB1424824A (en) 1976-02-11
US3834653A (en) 1974-09-10
DE2315280C2 (de) 1982-10-21
DE2315280A1 (de) 1973-10-11
JPS498000A (fr) 1974-01-24

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