GB8310161D0 - Adjusting position of earth satellite - Google Patents

Adjusting position of earth satellite

Info

Publication number
GB8310161D0
GB8310161D0 GB838310161A GB8310161A GB8310161D0 GB 8310161 D0 GB8310161 D0 GB 8310161D0 GB 838310161 A GB838310161 A GB 838310161A GB 8310161 A GB8310161 A GB 8310161A GB 8310161 D0 GB8310161 D0 GB 8310161D0
Authority
GB
United Kingdom
Prior art keywords
adjusting position
earth satellite
satellite
earth
adjusting
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
GB838310161A
Other versions
GB2121984B (en
GB2121984A (en
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
Mitsubishi Electric Corp
Original Assignee
Messerschmitt Bolkow Blohm AG
Mitsubishi Electric 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 Messerschmitt Bolkow Blohm AG, Mitsubishi Electric Corp filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB8310161D0 publication Critical patent/GB8310161D0/en
Publication of GB2121984A publication Critical patent/GB2121984A/en
Application granted granted Critical
Publication of GB2121984B publication Critical patent/GB2121984B/en
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
    • B64G1/32—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
    • B64G1/244—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
    • B64G1/28—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
    • B64G1/28—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
GB08310161A 1982-04-20 1983-04-14 Method of and equipment for adjusting the position of an earth satellite Expired GB2121984B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19823214373 DE3214373A1 (en) 1982-04-20 1982-04-20 METHOD AND DEVICE FOR THE POSITION CONTROL OF A SATELLITE

Publications (3)

Publication Number Publication Date
GB8310161D0 true GB8310161D0 (en) 1983-05-18
GB2121984A GB2121984A (en) 1984-01-04
GB2121984B GB2121984B (en) 1986-01-29

Family

ID=6161257

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08310161A Expired GB2121984B (en) 1982-04-20 1983-04-14 Method of and equipment for adjusting the position of an earth satellite

Country Status (4)

Country Link
JP (1) JPS58183395A (en)
DE (1) DE3214373A1 (en)
FR (1) FR2525359B1 (en)
GB (1) GB2121984B (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3606636C1 (en) * 1986-02-28 1987-11-05 Messerschmitt Boelkow Blohm Method for determining geomagnetic field components with reference to a satellite-fixed coordinate system
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
DE4007497A1 (en) * 1990-03-09 1991-09-12 Messerschmitt Boelkow Blohm Space station position control arrangement - contains electrically-driven reaction wheels and pivotable magnetic moment controllers for compensating disturbance moments
FR2670745B1 (en) * 1990-12-21 1993-04-16 Aerospatiale ATTITUDE CONTROL SYSTEM FOR 3-AXIS STABILIZED SATELLITE ON LOW TILT ORBIT.
FR2678894B1 (en) * 1991-07-09 1993-11-19 Aerospatiale Ste Nationale Indle METHOD AND DEVICE FOR CONTROLLING ATTITUDE IN A ROLL-LACET OF A SATELLITE WITH SINGLE DIRECTION OF CONTINUOUS ACTUATION.
CA2080612A1 (en) * 1991-11-27 1993-05-28 Douglas J. Bender Method and apparatus for compensating for magnetic disturbance torques on a satellite
FR2718105B1 (en) * 1994-03-30 1996-06-14 Centre Nat Etd Spatiales Artificial satellite provided with magnetic and aerodynamic moment generators and method for controlling such a satellite.
FR2724364B1 (en) * 1994-09-12 1997-01-17 Matra Marconi Space France METHOD AND SYSTEM FOR THREE-AXIS STABILIZATION OF A NON-EQUATORIAL ORBIT SATELLITE
DE19520115A1 (en) * 1995-06-01 1996-12-05 Contraves Gmbh Method for determining the roll position of a rolling flying object
JP5595978B2 (en) * 2011-05-28 2014-09-24 双葉電子工業株式会社 Drive control device for remote control equipment
CN108021138B (en) * 2017-11-03 2020-05-19 西北工业大学 Simplified design method of geomagnetic field model

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3189298A (en) * 1962-08-06 1965-06-15 Westinghouse Electric Corp Control apparatus for spacecraft
US3834653A (en) * 1972-03-27 1974-09-10 Rca Corp Closed loop roll and yaw control for satellites
CA1073988A (en) * 1975-07-21 1980-03-18 Ludwig Muhlfelder Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbits
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
JPS5628100A (en) * 1979-08-15 1981-03-19 Mitsubishi Electric Corp Wheel unloading device
JPS56131500A (en) * 1980-03-21 1981-10-15 Mitsubishi Electric Corp Magnetic controlling system for triaxes controlling satellite
US4521855A (en) * 1981-07-27 1985-06-04 Ford Aerospace & Communications Corporation Electronic on-orbit roll/yaw satellite control

Also Published As

Publication number Publication date
FR2525359A1 (en) 1983-10-21
GB2121984B (en) 1986-01-29
JPH0468199B2 (en) 1992-10-30
DE3214373C2 (en) 1987-10-15
FR2525359B1 (en) 1990-03-30
GB2121984A (en) 1984-01-04
JPS58183395A (en) 1983-10-26
DE3214373A1 (en) 1983-10-27

Similar Documents

Publication Publication Date Title
JPS56131498A (en) Structure for satellite
JPS5732146A (en) Ground station for earth satellite
JPS57136830A (en) Communication satellite
FR2550757B1 (en) SATELLITE POSITION REGULATION
GB2125633B (en) Antenna construction
GB8310161D0 (en) Adjusting position of earth satellite
GB8313955D0 (en) Satellite ground station
DE3377519D1 (en) Solid state compass
GB8528439D0 (en) Estimation of g/t of satellite earth terminals
GB8312889D0 (en) Satellite communications
GB8308107D0 (en) Surveying region of soil
GB8310476D0 (en) Magnetically adjusting position of satellite
GB2129280B (en) Watchband attachment structure
GB8310294D0 (en) Adjusting position of earth satellite
GB8531798D0 (en) Satellite navigation receiver
GB2127061B (en) Earth anchors
GB2115856B (en) Earth anchor
GB2122236B (en) Ground anchor
DE3372626D1 (en) Precipitation of polycycloolefins
KR840000459Y1 (en) Orienting adjuster of cock
GB2132659B (en) Ground anchor
GB8307387D0 (en) Ground-based structures
GB8513227D0 (en) Automatically tracking satellite
GB2119613B (en) Ploughs
IE821664L (en) Internally stabilized earth structure

Legal Events

Date Code Title Description
PE20 Patent expired after termination of 20 years

Effective date: 20030413