JP2004196290A5 - - Google Patents
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- JP2004196290A5 JP2004196290A5 JP2003416893A JP2003416893A JP2004196290A5 JP 2004196290 A5 JP2004196290 A5 JP 2004196290A5 JP 2003416893 A JP2003416893 A JP 2003416893A JP 2003416893 A JP2003416893 A JP 2003416893A JP 2004196290 A5 JP2004196290 A5 JP 2004196290A5
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- JP
- Japan
- 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.)
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Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/318,867 | 2002-12-13 | ||
| US10/318,867 US6990396B2 (en) | 2002-12-13 | 2002-12-13 | Method and apparatus for reaction wheel dynamic compensation in long-duration deployment of a large reflector |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2004196290A JP2004196290A (ja) | 2004-07-15 |
| JP2004196290A5 true JP2004196290A5 (ja) | 2005-09-29 |
| JP4969020B2 JP4969020B2 (ja) | 2012-07-04 |
Family
ID=32325982
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2003416893A Expired - Fee Related JP4969020B2 (ja) | 2002-12-13 | 2003-12-15 | 衛星から付属装置を展開しながら衛星の姿勢を制御する方法及び装置 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US6990396B2 (ja) |
| EP (1) | EP1428754B1 (ja) |
| JP (1) | JP4969020B2 (ja) |
| DE (1) | DE60301117T2 (ja) |
Families Citing this family (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7149610B2 (en) * | 2003-08-26 | 2006-12-12 | The Boeing Company | Momentum estimator for on-station momentum control |
| US7185858B2 (en) * | 2003-11-26 | 2007-03-06 | The Boeing Company | Spacecraft gyro calibration system |
| US7665695B2 (en) * | 2003-12-03 | 2010-02-23 | The Boeing Company | Unified attitude control for spacecraft transfer orbit operations |
| US20050133670A1 (en) * | 2003-12-03 | 2005-06-23 | Wang H. G. | Unified sensor-based attitude determination and control for spacecraft operations |
| US20080099626A1 (en) * | 2006-10-27 | 2008-05-01 | Goodrich Corporation | Reconfigurable reaction wheel for spacecraft |
| CN102012490B (zh) * | 2009-09-08 | 2013-05-22 | 上海卫星工程研究所 | 一种星载磁强计的支架结构 |
| US8561944B2 (en) * | 2010-06-17 | 2013-10-22 | Lockheed Martin Corporation | System and method for desaturation of a control moment gyroscope |
| US8800935B2 (en) * | 2011-03-09 | 2014-08-12 | Space Systems/Loral, Llc | Spacecraft payload positioning with respect to a virtual pivot point |
| FR2993863B1 (fr) * | 2012-07-27 | 2014-08-29 | Thales Sa | Procede de reduction du moment cinetique et de controle d'attitude d'un engin spatial |
| FR3010053B1 (fr) * | 2013-08-30 | 2016-10-21 | Thales Sa | Procede et dispositif de propulsion electrique de satellite |
| US9764858B2 (en) * | 2015-01-07 | 2017-09-19 | Mitsubishi Electric Research Laboratories, Inc. | Model predictive control of spacecraft |
| US9889950B2 (en) | 2015-02-20 | 2018-02-13 | Space Systems/Loral, Llc | Spacecraft with aerodynamic control |
| KR101640720B1 (ko) * | 2015-12-17 | 2016-07-18 | 한국항공우주연구원 | 위성 자세 제어 성능 비교 방법 및 장치 |
| CN106383523B (zh) * | 2016-09-30 | 2019-03-08 | 湖北航天技术研究院总体设计所 | 一种飞行器非线性姿态控制系统稳定性分析方法 |
| IT201900019322A1 (it) * | 2019-10-18 | 2021-04-18 | Thales Alenia Space Italia Spa Con Unico Socio | Assistenza end-to-end in orbita |
| CN111017268B (zh) * | 2019-12-09 | 2022-06-24 | 上海航天控制技术研究所 | 一种空间站对称舱段太阳翼协同控制系统及其控制方法 |
| WO2022197797A1 (en) * | 2021-03-16 | 2022-09-22 | Ast & Science Llc | Momentum wheels and reaction wheels for objects in space |
| CN113536550B (zh) * | 2021-06-29 | 2024-01-12 | 中国人民解放军63920部队 | 态势图生成方法、装置、非易失性存储介质及处理器 |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4325124A (en) | 1979-02-28 | 1982-04-13 | Organisation Europeenne De Recherches Spatiales | System for controlling the direction of the momentum vector of a geosynchronous satellite |
| US4306692A (en) | 1979-03-16 | 1981-12-22 | Communications Satellite Corporation | Attitude acquisition maneuver for a bias momentum spacecraft |
| JPS63125498A (ja) * | 1986-11-14 | 1988-05-28 | 三菱電機株式会社 | 人工衛星の姿勢制御装置 |
| JPH01275300A (ja) * | 1988-04-28 | 1989-11-02 | Nec Corp | 太陽輻射圧による宇宙飛翔体の姿勢制御法 |
| US4949922A (en) | 1988-12-09 | 1990-08-21 | Hughes Aircraft Company | Satellite control system |
| FR2669887B1 (fr) * | 1990-11-30 | 1995-06-02 | Aerospatiale | Procede de controle d'attitude en tangage d'un satellite grace a la pression de radiation solaire et satellite adapte a sa mise en óoeuvre. |
| JPH0717496A (ja) * | 1993-07-07 | 1995-01-20 | Fujitsu Ltd | 人工衛星の姿勢制御方式 |
| US6017000A (en) | 1998-08-02 | 2000-01-25 | Scott; David R. | Apparatus and methods for in-space satellite operations |
| JP3366095B2 (ja) * | 1994-02-10 | 2003-01-14 | 宇宙開発事業団 | 人工衛星の外乱トルク推定装置 |
| US5816540A (en) | 1995-12-22 | 1998-10-06 | Hughes Electronics | Optimal solar tracking system |
| US5906339A (en) | 1996-11-07 | 1999-05-25 | Motorola, Inc. | Multiple axis solar sailing |
| US6032903A (en) | 1998-02-12 | 2000-03-07 | Hughes Electronics Corporation | Cooperative control structures and methods for satellite spin axis control |
| US6138953A (en) * | 1998-03-02 | 2000-10-31 | Hughes Electronics Corporation | Slew rate direction determination for acquisition maneuvers using reaction wheels |
| US6076773A (en) | 1998-04-10 | 2000-06-20 | Hughes Electronics Corporation | Spin-stabilized spacecraft and methods |
| US6463365B1 (en) | 2000-02-01 | 2002-10-08 | Raytheon Company | System and method for controlling the attitude of a space craft |
-
2002
- 2002-12-13 US US10/318,867 patent/US6990396B2/en not_active Expired - Fee Related
-
2003
- 2003-12-11 EP EP03028384A patent/EP1428754B1/en not_active Expired - Fee Related
- 2003-12-11 DE DE60301117T patent/DE60301117T2/de not_active Expired - Lifetime
- 2003-12-15 JP JP2003416893A patent/JP4969020B2/ja not_active Expired - Fee Related