DE1948760A1 - Vorrichtung zur Steuerung der Haltung eines Raumsatelliten unter Verwendung des geomagnetischen Feldes - Google Patents
Vorrichtung zur Steuerung der Haltung eines Raumsatelliten unter Verwendung des geomagnetischen FeldesInfo
- Publication number
- DE1948760A1 DE1948760A1 DE19691948760 DE1948760A DE1948760A1 DE 1948760 A1 DE1948760 A1 DE 1948760A1 DE 19691948760 DE19691948760 DE 19691948760 DE 1948760 A DE1948760 A DE 1948760A DE 1948760 A1 DE1948760 A1 DE 1948760A1
- Authority
- DE
- Germany
- Prior art keywords
- satellite
- simulator
- vector
- coil
- attitude
- 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.)
- Pending
Links
- 230000005358 geomagnetic field Effects 0.000 title claims description 24
- 239000013598 vector Substances 0.000 claims description 93
- 230000033001 locomotion Effects 0.000 claims description 42
- 230000006870 function Effects 0.000 claims description 33
- 238000004088 simulation Methods 0.000 claims description 11
- 238000009434 installation Methods 0.000 claims description 9
- 238000004891 communication Methods 0.000 claims description 7
- 230000008859 change Effects 0.000 claims description 3
- 230000006399 behavior Effects 0.000 claims description 2
- 230000015572 biosynthetic process Effects 0.000 claims description 2
- 230000004075 alteration Effects 0.000 claims 1
- 230000005540 biological transmission Effects 0.000 claims 1
- 238000005755 formation reaction Methods 0.000 claims 1
- 208000021302 gastroesophageal reflux disease Diseases 0.000 claims 1
- 230000001360 synchronised effect Effects 0.000 claims 1
- 238000000034 method Methods 0.000 description 23
- 238000010586 diagram Methods 0.000 description 9
- 239000004020 conductor Substances 0.000 description 4
- 230000004907 flux Effects 0.000 description 3
- 238000004364 calculation method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 238000003722 High energy mechanical milling Methods 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005672 electromagnetic field Effects 0.000 description 1
- 238000011010 flushing procedure Methods 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000008707 rearrangement Effects 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 238000012549 training Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP43069505A JPS4913759B1 (enrdf_load_stackoverflow) | 1968-09-27 | 1968-09-27 | |
| JP43069504A JPS491439B1 (enrdf_load_stackoverflow) | 1968-09-27 | 1968-09-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE1948760A1 true DE1948760A1 (de) | 1970-05-06 |
Family
ID=26410690
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19691948760 Pending DE1948760A1 (de) | 1968-09-27 | 1969-09-26 | Vorrichtung zur Steuerung der Haltung eines Raumsatelliten unter Verwendung des geomagnetischen Feldes |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE1948760A1 (enrdf_load_stackoverflow) |
| FR (1) | FR2019068A1 (enrdf_load_stackoverflow) |
| GB (1) | GB1285919A (enrdf_load_stackoverflow) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2525360A1 (fr) * | 1982-04-20 | 1983-10-21 | Messerschmitt Boelkow Blohm | Procede et dispositif de regulation magnetique d'attitude d'un satellite artificiel |
| 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 |
| CN115817856A (zh) * | 2022-11-21 | 2023-03-21 | 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 |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| CN117040608B (zh) * | 2023-10-10 | 2023-12-08 | 四川轻化工大学 | 一种车载卫星中继 |
-
1969
- 1969-09-25 GB GB47227/69A patent/GB1285919A/en not_active Expired
- 1969-09-26 DE DE19691948760 patent/DE1948760A1/de active Pending
- 1969-09-26 FR FR6932990A patent/FR2019068A1/fr not_active Withdrawn
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2525360A1 (fr) * | 1982-04-20 | 1983-10-21 | Messerschmitt Boelkow Blohm | Procede et dispositif de regulation magnetique d'attitude d'un satellite artificiel |
| DE3214379A1 (de) * | 1982-04-20 | 1983-10-27 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Einrichtung fuer die magnetische lageregelung von satelliten |
| 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 |
| CN115817856A (zh) * | 2022-11-21 | 2023-03-21 | 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| GB1285919A (en) | 1972-08-16 |
| FR2019068A1 (enrdf_load_stackoverflow) | 1970-06-26 |
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