GB1285919A - A device for automatically controlling the attitude of a space satellite utilizing geomagnetic field - Google Patents

A device for automatically controlling the attitude of a space satellite utilizing geomagnetic field

Info

Publication number
GB1285919A
GB1285919A GB47227/69A GB4722769A GB1285919A GB 1285919 A GB1285919 A GB 1285919A GB 47227/69 A GB47227/69 A GB 47227/69A GB 4722769 A GB4722769 A GB 4722769A GB 1285919 A GB1285919 A GB 1285919A
Authority
GB
United Kingdom
Prior art keywords
satellite
attitude
computer
sensor
geomagnetic field
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
Application number
GB47227/69A
Other languages
English (en)
Inventor
Moritada Kubo
Masamichi Shigehara
Shozo Yasui
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.)
Toshiba Corp
Original Assignee
Tokyo Shibaura Electric Co Ltd
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
Priority claimed from JP43069504A external-priority patent/JPS491439B1/ja
Priority claimed from JP43069505A external-priority patent/JPS4913759B1/ja
Application filed by Tokyo Shibaura Electric Co Ltd filed Critical Tokyo Shibaura Electric Co Ltd
Publication of GB1285919A publication Critical patent/GB1285919A/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
    • B64G1/36—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
    • B64G1/24—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
    • 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
    • B64G1/361—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using star 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun 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
    • B64G1/36—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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/369—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using gyroscopes as attitude sensors

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
GB47227/69A 1968-09-27 1969-09-25 A device for automatically controlling the attitude of a space satellite utilizing geomagnetic field Expired GB1285919A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP43069504A JPS491439B1 (enrdf_load_html_response) 1968-09-27 1968-09-27
JP43069505A JPS4913759B1 (enrdf_load_html_response) 1968-09-27 1968-09-27

Publications (1)

Publication Number Publication Date
GB1285919A true GB1285919A (en) 1972-08-16

Family

ID=26410690

Family Applications (1)

Application Number Title Priority Date Filing Date
GB47227/69A Expired GB1285919A (en) 1968-09-27 1969-09-25 A device for automatically controlling the attitude of a space satellite utilizing geomagnetic field

Country Status (3)

Country Link
DE (1) DE1948760A1 (enrdf_load_html_response)
FR (1) FR2019068A1 (enrdf_load_html_response)
GB (1) GB1285919A (enrdf_load_html_response)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2129969A (en) * 1982-04-20 1984-05-23 Messerschmitt Boelkow Blohm Method of and apparatus for magnetically adjusting the position of a satellite
RU2332334C1 (ru) * 2006-10-24 2008-08-27 Кирилл Андреевич Антипов Способ полупассивной трехосной стабилизации динамически симметричного искусственного спутника земли
CN100441483C (zh) * 2006-12-14 2008-12-10 北京航空航天大学 一种集成化磁悬浮控制力矩陀螺控制平台
CN105173120A (zh) * 2015-09-21 2015-12-23 上海卫星工程研究所 卫星在轨自主实施作业任务的控制方法
CN105487402A (zh) * 2014-09-17 2016-04-13 上海新跃仪表厂 一种星敏与陀螺组合定姿全物理仿真试验方法
CN107054702A (zh) * 2017-02-15 2017-08-18 上海航天控制技术研究所 一种半物理仿真测试中地磁场模拟方法
CN111060111A (zh) * 2019-12-23 2020-04-24 北京国电高科科技有限公司 一种低轨卫星入轨初期定轨方法
CN116039972A (zh) * 2022-12-01 2023-05-02 北京微纳星空科技有限公司 一种卫星控制系统、方法、电子设备及存储介质
CN116714782A (zh) * 2023-07-09 2023-09-08 西北工业大学 金字塔型电磁编队的空间失效卫星非接触式变轨操控方法
CN117040608A (zh) * 2023-10-10 2023-11-10 四川轻化工大学 一种车载卫星中继

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3606636C1 (de) * 1986-02-28 1987-11-05 Messerschmitt Boelkow Blohm Verfahren zur Bestimmung von Erdmagnetfeldkomponenten bezueglich eines satellitenfesten Koordinatensystems
CN113581492B (zh) * 2021-07-23 2023-07-21 上海卫星工程研究所 应用于双星组合入轨角色自适应配置方法
CN115817856B (zh) * 2022-11-21 2023-06-20 清华大学 基于纯磁控方式的卫星对日自旋稳定姿态控制方法及装置

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2129969A (en) * 1982-04-20 1984-05-23 Messerschmitt Boelkow Blohm Method of and apparatus for magnetically adjusting the position of a satellite
RU2332334C1 (ru) * 2006-10-24 2008-08-27 Кирилл Андреевич Антипов Способ полупассивной трехосной стабилизации динамически симметричного искусственного спутника земли
CN100441483C (zh) * 2006-12-14 2008-12-10 北京航空航天大学 一种集成化磁悬浮控制力矩陀螺控制平台
CN105487402B (zh) * 2014-09-17 2018-07-20 上海新跃仪表厂 一种星敏与陀螺组合定姿全物理仿真试验方法
CN105487402A (zh) * 2014-09-17 2016-04-13 上海新跃仪表厂 一种星敏与陀螺组合定姿全物理仿真试验方法
CN105173120A (zh) * 2015-09-21 2015-12-23 上海卫星工程研究所 卫星在轨自主实施作业任务的控制方法
CN105173120B (zh) * 2015-09-21 2017-03-22 上海卫星工程研究所 卫星在轨自主实施作业任务的控制方法
CN107054702A (zh) * 2017-02-15 2017-08-18 上海航天控制技术研究所 一种半物理仿真测试中地磁场模拟方法
CN107054702B (zh) * 2017-02-15 2019-07-26 上海航天控制技术研究所 一种半物理仿真测试中地磁场模拟方法
CN111060111A (zh) * 2019-12-23 2020-04-24 北京国电高科科技有限公司 一种低轨卫星入轨初期定轨方法
CN116039972A (zh) * 2022-12-01 2023-05-02 北京微纳星空科技有限公司 一种卫星控制系统、方法、电子设备及存储介质
CN116714782A (zh) * 2023-07-09 2023-09-08 西北工业大学 金字塔型电磁编队的空间失效卫星非接触式变轨操控方法
CN117040608A (zh) * 2023-10-10 2023-11-10 四川轻化工大学 一种车载卫星中继
CN117040608B (zh) * 2023-10-10 2023-12-08 四川轻化工大学 一种车载卫星中继

Also Published As

Publication number Publication date
DE1948760A1 (de) 1970-05-06
FR2019068A1 (enrdf_load_html_response) 1970-06-26

Similar Documents

Publication Publication Date Title
GB1285919A (en) A device for automatically controlling the attitude of a space satellite utilizing geomagnetic field
US8213803B2 (en) Method and system for laser based communication
JP2625282B2 (ja) 宇宙船地球方向姿勢獲得方法
GB1408504A (en) Attitude stabilization system
US5957982A (en) Method and system for space navigation
US5193064A (en) Method and apparatus of integrating Global Positioning System and Inertial Navigation System without using accelerometers
US8186626B1 (en) GPS based orbit determination of a spacecraft in the presence of thruster maneuvers
US3681583A (en) Device for controlling the attitude of a space satellite utilizing geomagnetic field
US3241363A (en) Navigation instruments
US2963243A (en) Space vehicle guidance mechanism and method
US2561367A (en) Gyroscope control system
US12286242B2 (en) Magnetic control of spacecraft
US3747095A (en) Synchronous satellite tracking system
US3164340A (en) Inertial guidance system using vehicle fixed inertial elements
US4807835A (en) Spacecraft attitude stabilization system
GB1413658A (en) Solar torque compensation for a satellite or other spacecraft
US2949030A (en) Gyroscopically stabilized optical system platform
USRE29177E (en) Solar torque compensation for a satellite
US2887782A (en) Gyro magnetic compass system
US2429605A (en) Presetting means for long period gyroscopes
US3280642A (en) Directional gyroscope
Ninomiya et al. Magnetic torquing scheme for attitude control of a wheel-stabilized astronomy satellite
Hecht et al. Magnetic attitude control of the Tiros satellites
US3097816A (en) Attitude controls
US3377854A (en) Inertial platform trimming system

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
435 Patent endorsed 'licences of right' on the date specified (sect. 35/1949)
PE20 Patent expired after termination of 20 years