DE60109521T2 - Vorrichtung zur lageregelung eines raumfahrzeuges - Google Patents
Vorrichtung zur lageregelung eines raumfahrzeuges Download PDFInfo
- Publication number
- DE60109521T2 DE60109521T2 DE60109521T DE60109521T DE60109521T2 DE 60109521 T2 DE60109521 T2 DE 60109521T2 DE 60109521 T DE60109521 T DE 60109521T DE 60109521 T DE60109521 T DE 60109521T DE 60109521 T2 DE60109521 T2 DE 60109521T2
- Authority
- DE
- Germany
- Prior art keywords
- spacecraft
- axis
- payload
- reaction
- bus
- 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
Links
- 230000007246 mechanism Effects 0.000 claims description 17
- 239000000725 suspension Substances 0.000 claims description 10
- 230000004044 response Effects 0.000 claims description 5
- 150000001875 compounds Chemical class 0.000 claims description 2
- 230000001419 dependent effect Effects 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 8
- 238000000034 method Methods 0.000 description 6
- 238000004891 communication Methods 0.000 description 5
- 238000009987 spinning Methods 0.000 description 4
- 230000006641 stabilisation Effects 0.000 description 4
- 238000011105 stabilization Methods 0.000 description 4
- 238000001514 detection method Methods 0.000 description 3
- 239000000446 fuel Substances 0.000 description 3
- 230000006870 function Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 238000002955 isolation Methods 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000003466 anti-cipated effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000001575 pathological effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 238000013519 translation Methods 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
- B64G1/36—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
- B64G1/28—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
- B64G1/283—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
-
- 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)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US496140 | 2000-02-01 | ||
| US09/496,140 US6463365B1 (en) | 2000-02-01 | 2000-02-01 | System and method for controlling the attitude of a space craft |
| PCT/US2001/003314 WO2001056882A1 (en) | 2000-02-01 | 2001-02-01 | System and method for controlling the attitude of a spacecraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE60109521D1 DE60109521D1 (de) | 2005-04-28 |
| DE60109521T2 true DE60109521T2 (de) | 2006-02-16 |
Family
ID=23971402
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE60109521T Expired - Lifetime DE60109521T2 (de) | 2000-02-01 | 2001-02-01 | Vorrichtung zur lageregelung eines raumfahrzeuges |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US6463365B1 (https=) |
| EP (1) | EP1165371B1 (https=) |
| JP (1) | JP4550347B2 (https=) |
| DE (1) | DE60109521T2 (https=) |
| IL (1) | IL145416A (https=) |
| WO (1) | WO2001056882A1 (https=) |
Families Citing this family (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0203950D0 (en) * | 2002-02-20 | 2002-04-03 | Astrium Ltd | Method and system for balancing thrust demands |
| US6648274B1 (en) * | 2002-04-12 | 2003-11-18 | David A. Bailey | Virtual reaction wheel array |
| AU2003247873A1 (en) * | 2002-07-16 | 2004-02-02 | The Charles Stark Draper Laboratory, Inc. | Integrated inertial stellar attitude sensor |
| US6990396B2 (en) * | 2002-12-13 | 2006-01-24 | The Boeing Company | Method and apparatus for reaction wheel dynamic compensation in long-duration deployment of a large reflector |
| US7025307B2 (en) * | 2002-12-13 | 2006-04-11 | The Boeing Company | Method and apparatus for solar tacking momentum maintenance in long-duration deployment of a large reflector |
| US7437222B2 (en) * | 2005-07-28 | 2008-10-14 | The Boeing Company | Gimbal disturbance calibration and compenstion |
| EP1813957B1 (fr) * | 2006-01-19 | 2010-03-10 | Thales | Dispositif de contrôle de position(s) relative(s) par analyse de signaux bi-fréquences, pour un engin spatial d'un groupe d'engins spatiaux en formation |
| US8019493B1 (en) * | 2007-07-20 | 2011-09-13 | Lockheed Martin Corporation | Spacecraft thruster torque feedforward calibration system |
| KR101008176B1 (ko) * | 2008-12-30 | 2011-01-13 | 한국항공우주연구원 | 반작용휠과 추력기 기반 자세제어기를 동시에 이용한 자세기동 및 가제어성 향상 방법 |
| WO2011100482A2 (en) * | 2010-02-10 | 2011-08-18 | Scott Gregory Dietz | Motorized apparatus and moment imparting device |
| US10192173B2 (en) | 2010-07-02 | 2019-01-29 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | System and method for training of state-classifiers |
| US8640994B1 (en) * | 2010-09-27 | 2014-02-04 | The Boeing Company | Agile dedicated spacecraft for spinning microwave imagers and sounders |
| US9764858B2 (en) * | 2015-01-07 | 2017-09-19 | Mitsubishi Electric Research Laboratories, Inc. | Model predictive control of spacecraft |
| RU2594056C1 (ru) * | 2015-02-02 | 2016-08-10 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Способ одноосной ориентации космического аппарата вытянутой формы |
| RU2594057C1 (ru) * | 2015-02-02 | 2016-08-10 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Способ одноосной ориентации космического аппарата вытянутой формы |
| RU2594054C1 (ru) * | 2015-02-02 | 2016-08-10 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Способ одноосной ориентации космического аппарата вытянутой формы |
| CN106484929B (zh) * | 2015-08-26 | 2019-06-28 | 上海宇航系统工程研究所 | 一种月球探测航天器多状态转动惯量计算方法 |
| CN105843244A (zh) * | 2016-06-02 | 2016-08-10 | 北京航空航天大学 | 一种基于输出反馈的挠性航天器精细姿态控制方法 |
| JP2020062951A (ja) * | 2018-10-17 | 2020-04-23 | 富士通株式会社 | 飛翔機 |
| US11279501B2 (en) * | 2018-10-25 | 2022-03-22 | General Atomics | Satellite attitude control system using eigen vector, non-linear dynamic inversion, and feedforward control |
| US12172660B2 (en) | 2021-03-03 | 2024-12-24 | United States Of America As Represented By The Administrator Of Nasa | Method and system for collaborative task-based allocation between human and autonomous systems |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0134288B1 (de) * | 1983-09-03 | 1988-05-11 | ERNO Raumfahrttechnik Gesellschaft mit beschränkter Haftung | Variabel konfigurierbares Satellitensystem |
| US4723735A (en) * | 1984-12-28 | 1988-02-09 | The Charles Stark Draper Laboratory, Inc. | Energy storage attitude control and reference system |
| US4824052A (en) * | 1987-06-18 | 1989-04-25 | Hughes Aircraft Company | Nutation sensor and nutation control system for a dual-spin stabilized satellite |
| US5067673A (en) * | 1990-02-07 | 1991-11-26 | Hughes Aircraft Company | Essentially passive method for inverting the orientation of a dual spin spacecraft |
| US5131611A (en) * | 1991-04-26 | 1992-07-21 | The Perkin-Elmer Corporation | Method and apparatus for reactionless rotation |
| US5441222A (en) * | 1993-04-26 | 1995-08-15 | Hughes Aircraft Company | Attitude control of spinning spacecraft |
| US5667171A (en) * | 1995-04-28 | 1997-09-16 | Hughes Aircraft Company | Satellite spin axis stabilization using a single degree of freedom transverse momentum storage device |
| US5751078A (en) * | 1996-10-03 | 1998-05-12 | Lockheed Martin Corp. Missiles & Space | Reactionless, momentum compensated payload positioner |
| US6068218A (en) * | 1997-05-14 | 2000-05-30 | Hughes Electronics Corporation | Agile, spinning spacecraft with sun-steerable solar cell array and method |
| US6152402A (en) * | 1999-04-07 | 2000-11-28 | Hughes Electronics Corporation | Dual spin zero momentum satellite system |
-
2000
- 2000-02-01 US US09/496,140 patent/US6463365B1/en not_active Expired - Lifetime
-
2001
- 2001-02-01 DE DE60109521T patent/DE60109521T2/de not_active Expired - Lifetime
- 2001-02-01 EP EP01910400A patent/EP1165371B1/en not_active Expired - Lifetime
- 2001-02-01 IL IL14541601A patent/IL145416A/xx active IP Right Grant
- 2001-02-01 WO PCT/US2001/003314 patent/WO2001056882A1/en not_active Ceased
- 2001-02-01 JP JP2001556743A patent/JP4550347B2/ja not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JP2003521424A (ja) | 2003-07-15 |
| US6463365B1 (en) | 2002-10-08 |
| DE60109521D1 (de) | 2005-04-28 |
| JP4550347B2 (ja) | 2010-09-22 |
| IL145416A (en) | 2005-03-20 |
| EP1165371A1 (en) | 2002-01-02 |
| WO2001056882A1 (en) | 2001-08-09 |
| IL145416A0 (en) | 2002-06-30 |
| EP1165371B1 (en) | 2005-03-23 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 8364 | No opposition during term of opposition |