DE3879910D1 - System zur bestimmung und steuerung der lage eines satelliten mit einem in richtung steuerbaren sensorsbuendel. - Google Patents
System zur bestimmung und steuerung der lage eines satelliten mit einem in richtung steuerbaren sensorsbuendel.Info
- Publication number
- DE3879910D1 DE3879910D1 DE8888710057T DE3879910T DE3879910D1 DE 3879910 D1 DE3879910 D1 DE 3879910D1 DE 8888710057 T DE8888710057 T DE 8888710057T DE 3879910 T DE3879910 T DE 3879910T DE 3879910 D1 DE3879910 D1 DE 3879910D1
- Authority
- DE
- Germany
- Prior art keywords
- satellite
- determining
- controlling
- sensor bundle
- directionally controllable
- 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
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
-
- 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
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)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/137,225 US4883244A (en) | 1987-12-23 | 1987-12-23 | Satellite attitude determination and control system with agile beam sensing |
Publications (2)
Publication Number | Publication Date |
---|---|
DE3879910D1 true DE3879910D1 (de) | 1993-05-06 |
DE3879910T2 DE3879910T2 (de) | 1993-10-14 |
Family
ID=22476361
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE88710057T Expired - Lifetime DE3879910T2 (de) | 1987-12-23 | 1988-12-23 | System zur Bestimmung und Steuerung der Lage eines Satelliten mit einem in Richtung steuerbaren Sensorsbündel. |
Country Status (5)
Country | Link |
---|---|
US (1) | US4883244A (de) |
EP (1) | EP0322349B1 (de) |
JP (1) | JP2588958B2 (de) |
CA (1) | CA1318011C (de) |
DE (1) | DE3879910T2 (de) |
Families Citing this family (47)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5092543A (en) * | 1989-09-27 | 1992-03-03 | General Electric Company | Spacecraft attitude control with avoidance constraint |
US7417584B1 (en) * | 1989-11-08 | 2008-08-26 | Lockheed Martin Corporation | Monopulse radar estimation of target altitude at low angles of elevation |
US5048774A (en) * | 1989-12-20 | 1991-09-17 | Barnes Engineering Co. | High-accuracy attitude sensor for spin stabilized satellite |
US5100084A (en) * | 1990-04-16 | 1992-03-31 | Space Systems/Loral, Inc. | Method and apparatus for inclined orbit attitude control for momentum bias spacecraft |
US5204818A (en) * | 1990-05-22 | 1993-04-20 | The United States Of America As Represented By The Secretary Of The Air Force | Surveying satellite apparatus |
US5043737A (en) * | 1990-06-05 | 1991-08-27 | Hughes Aircraft Company | Precision satellite tracking system |
US5184139A (en) * | 1990-08-29 | 1993-02-02 | Kabushiki Kaisha Toshiba | Antenna pointing equipment |
US5051751A (en) * | 1991-02-12 | 1991-09-24 | The United States Of America As Represented By The Secretary Of The Navy | Method of Kalman filtering for estimating the position and velocity of a tracked object |
US5762298A (en) * | 1991-03-27 | 1998-06-09 | Chen; Franklin Y. K. | Use of artificial satellites in earth orbits adaptively to modify the effect that solar radiation would otherwise have on earth's weather |
US5175556A (en) * | 1991-06-07 | 1992-12-29 | General Electric Company | Spacecraft antenna pattern control system |
DE4135034C2 (de) * | 1991-10-23 | 1995-04-13 | Deutsche Forsch Luft Raumfahrt | Einrichtung zur Bahnkontrolle von mindestens zwei kopositionierten geostationären Satelliten |
US5311435A (en) * | 1991-11-27 | 1994-05-10 | Hughes Aircraft Company | Method for station keeping control of flexible spacecraft using onboard gain scheduling scheme |
CA2080612A1 (en) * | 1991-11-27 | 1993-05-28 | Douglas J. Bender | Method and apparatus for compensating for magnetic disturbance torques on a satellite |
DE4243395C2 (de) * | 1991-12-21 | 1997-05-22 | Deutsche Forsch Luft Raumfahrt | Anordnung zur koordinierten Positionshaltung eines geostationären Satellitenschwarms |
US5546309A (en) * | 1993-10-20 | 1996-08-13 | The Charles Stark Draper Laboratory, Inc. | Apparatus and method for autonomous satellite attitude sensing |
US5587714A (en) * | 1995-03-10 | 1996-12-24 | Space Systems/Loral, Inc. | Spacecraft antenna pointing error correction |
US5758260A (en) * | 1995-08-23 | 1998-05-26 | Globalstar L.P. | Satellite beam steering reference using terrestrial beam steering terminals |
US5917447A (en) * | 1996-05-29 | 1999-06-29 | Motorola, Inc. | Method and system for digital beam forming |
US6138061A (en) * | 1997-04-18 | 2000-10-24 | Hughes Electronics Corporation | Onboard orbit propagation using quaternions |
US6113034A (en) * | 1997-08-04 | 2000-09-05 | Motorola, Inc. | Method and apparatus for estimating effects of disturbance forces |
US5959576A (en) * | 1997-08-12 | 1999-09-28 | Honeywell Inc. | Satellite attitude determination using GPS and intersatellite line of sight communications |
US6085128A (en) * | 1998-02-06 | 2000-07-04 | The United States Of America As Represented By The Secretary Of The Navy | Orbit/covariance estimation and analysis (OCEAN) determination for satellites |
FR2774828B1 (fr) * | 1998-02-06 | 2000-04-21 | Centre Nat Etd Spatiales | Systeme spatial de telecommunications comprenant au moins un satellite, et procede de synchronisation d'un tel systeme |
US6195044B1 (en) | 1998-06-19 | 2001-02-27 | Hughes Electronics Corporation | Laser crosslink satellite attitude determination system and method |
US6219593B1 (en) * | 1999-03-01 | 2001-04-17 | Motorola, Inc. | Method and apparatus for attitude determination in a multi-nodal system |
DE19924908B4 (de) * | 1999-05-31 | 2008-05-29 | Astrium Gmbh | Verfahren zur dreiachsigen Lagebestimmung für einen niedrig fliegenden Satelliten |
US6184825B1 (en) * | 1999-06-29 | 2001-02-06 | Trw Inc. | Method and apparatus for radio frequency beam pointing |
US6142423A (en) * | 1999-06-29 | 2000-11-07 | Trw Inc. | Ephemeris/attitude reference determination using on-board optics and other satellite ephemeris |
JP3566628B2 (ja) * | 2000-06-30 | 2004-09-15 | 三菱電機株式会社 | 衛星捕捉方法 |
JP3858574B2 (ja) | 2000-09-01 | 2006-12-13 | 日本電気株式会社 | 人工衛星のオフライン広帯域姿勢検出装置及びその方法 |
US6695262B2 (en) | 2001-12-07 | 2004-02-24 | The Boeing Company | Spacecraft methods and structures for enhanced service-attitude accuracy |
US6735524B1 (en) | 2002-12-10 | 2004-05-11 | The Boeing Company | Spatially resolved and spatially aware antenna for radio navigation |
US7134630B2 (en) * | 2004-08-30 | 2006-11-14 | The Boeing Company | Thermal deformation determination for payload pointing using space-based beacon |
US7663542B1 (en) * | 2004-11-04 | 2010-02-16 | Lockheed Martin Corporation | Antenna autotrack control system for precision spot beam pointing control |
US8706322B2 (en) * | 2006-06-20 | 2014-04-22 | Kara Whitney Johnson | Method and computer program product for controlling inertial attitude of an artificial satellite by applying gyroscopic precession to maintain the spin axis perpendicular to sun lines |
US8634974B2 (en) * | 2012-01-09 | 2014-01-21 | Google Inc. | Using predicted movement to maintain optical-communication lock with nearby balloon |
US8686721B2 (en) | 2012-02-27 | 2014-04-01 | The Johns Hopkins University | Automated pre-processing of body-mounted magnetometer data from constellations of low earth orbit satellites for derivation of birkeland current signatures |
CN103600852B (zh) * | 2013-11-25 | 2015-10-07 | 清华大学 | 支持集群飞行的基础模块航天器 |
US20170272149A1 (en) * | 2014-11-28 | 2017-09-21 | Paris Michaels | Inter-satellite space communication system - method and apparatus |
CN106950975B (zh) * | 2017-01-24 | 2019-05-31 | 上海卫星工程研究所 | 大角度机动高分辨率微波遥感卫星总体控制方法 |
CN109742543B (zh) * | 2019-01-29 | 2021-07-23 | 上海微小卫星工程中心 | 一种用于将终端的天线对准卫星的方法及相应系统 |
CN113382931A (zh) * | 2019-01-31 | 2021-09-10 | 优鲁格斯股份有限公司 | 姿态控制系统和方法 |
US11124320B2 (en) * | 2019-02-12 | 2021-09-21 | Canadian Space Agency | Spacecraft control using residual dipole |
US10925114B1 (en) | 2019-11-11 | 2021-02-16 | Loon Llc | Remote monitoring of geographically distributed assets using mobile platforms |
US20230093716A1 (en) * | 2021-09-20 | 2023-03-23 | WildStar, LLC | Satellite and antenna therefor |
CN114201865A (zh) * | 2021-12-02 | 2022-03-18 | 北京理工大学 | 集成卫星轨道位姿的光学载荷外部杂散光仿真分析方法 |
CN117485595B (zh) * | 2023-11-21 | 2024-04-05 | 北京易动宇航科技有限公司 | 一种用于电推进系统的能量管理方法 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3061239A (en) * | 1960-08-04 | 1962-10-30 | Lockheed Aircraft Corp | Magnetic moment device for applying corrective torque to a space vehicle |
US3341151A (en) * | 1965-07-23 | 1967-09-12 | Kampinsky Abe | Apparatus providing a directive field pattern and attitude sensing of a spin stabilized satellite |
US3390847A (en) * | 1966-05-19 | 1968-07-02 | Air Force Usa | Earth's orientation of satellite antenna |
FR2044517A5 (de) * | 1969-05-23 | 1971-02-19 | Compteurs Comp D | |
US3949400A (en) * | 1973-11-28 | 1976-04-06 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Position determination systems |
GB2015292B (en) * | 1977-11-30 | 1982-06-23 | Wright T | Method for determining the attitude of a spinning spacecraft |
BE877989A (fr) * | 1979-07-31 | 1979-11-16 | Organisation Europ De Rech S S | Systeme de controle d'attitude d'un engin spatial |
US4405986A (en) * | 1981-04-17 | 1983-09-20 | The United States Of America As Represented By The Secretary Of The Army | GSP/Doppler sensor velocity derived attitude reference system |
US4599619A (en) * | 1982-07-13 | 1986-07-08 | Rca Corporation | Satellite dual antenna pointing system |
US4617634A (en) * | 1983-06-28 | 1986-10-14 | Mitsubishi Denki Kabushiki Kaisha | Artificial satellite attitude control system |
FR2605427A1 (fr) * | 1986-10-16 | 1988-04-22 | Centre Nat Etd Spatiales | Pointage d'une antenne de sonde spatiale vers la terre |
-
1987
- 1987-12-23 US US07/137,225 patent/US4883244A/en not_active Expired - Lifetime
-
1988
- 1988-12-20 CA CA000586390A patent/CA1318011C/en not_active Expired - Lifetime
- 1988-12-23 DE DE88710057T patent/DE3879910T2/de not_active Expired - Lifetime
- 1988-12-23 JP JP63325739A patent/JP2588958B2/ja not_active Expired - Lifetime
- 1988-12-23 EP EP88710057A patent/EP0322349B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JP2588958B2 (ja) | 1997-03-12 |
US4883244A (en) | 1989-11-28 |
CA1318011C (en) | 1993-05-18 |
EP0322349A3 (en) | 1990-06-13 |
DE3879910T2 (de) | 1993-10-14 |
EP0322349A2 (de) | 1989-06-28 |
JPH01204899A (ja) | 1989-08-17 |
EP0322349B1 (de) | 1993-03-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: HUGHES ELECTRONICS CORP., EL SEGUNDO, CALIF., US |
|
8328 | Change in the person/name/address of the agent |
Representative=s name: WITTE, WELLER & PARTNER, 70178 STUTTGART |