JP2013095416A - サービスを提供するよう適合された少なくとも2つの衛星からなる1組の衛星を制御する方法およびシステム - Google Patents
サービスを提供するよう適合された少なくとも2つの衛星からなる1組の衛星を制御する方法およびシステム Download PDFInfo
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- 238000004891 communication Methods 0.000 claims description 6
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- 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
- B64G1/242—Orbits and trajectories
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/1085—Swarms and constellations
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- 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
- B64G1/242—Orbits and trajectories
- B64G1/2429—Station keeping
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
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- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/1851—Systems using a satellite or space-based relay
- H04B7/18519—Operations control, administration or maintenance
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/1007—Communications satellites
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/1021—Earth observation satellites
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Abstract
【解決手段】 本発明は、サービスを提供するよう適合された少なくとも2つの衛星からなる1組の衛星を制御するための方法であって、サービスは、所定の瞬間に前記1組の衛星の少なくとも一部によって使用される方法であり、連続的または疑似連続的に、各衛星のそれぞれの昇交点赤経(Ωi(t))の平均値(ΩM(t))が計算され、各衛星に対し、前記現時点における平均値(ΩM(t))と等しいセットポイント上での昇交点赤経(Ωi(t))の調整によって衛星の軌道の修正が適用される方法に関する。
【選択図】 図2
Description
22 工程
Claims (7)
- サービスを提供するよう適合された少なくとも2つの衛星からなる1組の衛星を制御するための方法であって、前記サービスは、所定の瞬間に前記1組の衛星の少なくとも一部によって使用される、方法であり、連続的または疑似連続的に、各衛星のそれぞれの昇交点赤経(Ωi(t))の平均値(ΩM(t))が計算され、各衛星に対し、前記現時点における平均値(ΩM(t))と等しいセットポイント上での前記昇交点赤経(Ωi(t))の調整によって前記衛星の軌道の修正が制御される、方法。
- 前記衛星の前記昇交点赤経(Ωi(t))はそれぞれ、衛星がその地上管制局から見える所に位置する際に測定される、請求項1に記載の方法。
- 前記地上管制局は、通信ネットワークを介して接続される、請求項2に記載の方法。
- 単一の地上管制局は、前記1組の衛星に対して使用される、請求項1〜3のいずれか一項に記載の方法。
- 前記衛星が前記サービスの提供に参加する際に適用される衛星の前記軌道を修正するための制御は、もはや前記衛星が前記サービスの提供に参加しなくなる瞬間まで保留することができる、請求項1〜4のいずれか一項に記載の方法。
- 前記計算および制御は、前記1組の衛星によって自律的に行われ、後者は、前記平均値の前記計算に必要なそれらの昇交点赤経値を同報通信するため、任意選択的に、互いに通信し合うことができる、請求項1に記載の方法。
- サービスを提供するよう適合された少なくとも2つの衛星からなる1組の衛星(S1、S2、S3)を制御するためのシステムであって、前記サービスは、所定の瞬間に前記1組の衛星の少なくとも一部によって使用されるシステムであり、連続的または疑似連続的に、各衛星のそれぞれの昇交点赤経(Ωi(t))の平均値(ΩM(t))を計算するための手段と、各衛星に対し、前記現時点における平均値(ΩM(t))と等しいセットポイント上での前記昇交点赤経(Ωi(t))の調整によって前記衛星の軌道の修正を制御する手段とを備える、システム。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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FR1103290 | 2011-10-28 | ||
FR1103290A FR2982045B1 (fr) | 2011-10-28 | 2011-10-28 | Procede et systeme de commande d'un ensemble d'au moins deux satellites adaptes pour fournir un service |
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JP2013095416A true JP2013095416A (ja) | 2013-05-20 |
JP2013095416A5 JP2013095416A5 (ja) | 2017-08-17 |
JP6199021B2 JP6199021B2 (ja) | 2017-09-20 |
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JP2012235542A Active JP6199021B2 (ja) | 2011-10-28 | 2012-10-25 | サービスを提供するよう適合された少なくとも2つの衛星からなる1組の衛星を制御する方法およびシステム |
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US (1) | US8783620B2 (ja) |
EP (1) | EP2586711B1 (ja) |
JP (1) | JP6199021B2 (ja) |
CA (1) | CA2792580C (ja) |
DK (1) | DK2586711T3 (ja) |
ES (1) | ES2538093T3 (ja) |
FR (1) | FR2982045B1 (ja) |
RU (1) | RU2608186C2 (ja) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
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US9309010B2 (en) * | 2014-01-10 | 2016-04-12 | The Boeing Company | Methods and apparatus for controlling a plurality of satellites using node-synchronous eccentricity control |
US10053241B2 (en) * | 2016-12-01 | 2018-08-21 | The Boeing Company | Systems and methods for multi-spacecraft distributed ascent |
US20180155066A1 (en) * | 2016-12-01 | 2018-06-07 | Electronics And Telecommunications Research Institute | Method and apparatus for controlling orbit of collocated satellite |
CN108055069A (zh) * | 2017-12-11 | 2018-05-18 | 中国人民解放军战略支援部队航天工程大学 | 低轨通信和导航增强混合星座维持控制边界计算及控制方法 |
CN114715430B (zh) * | 2021-03-31 | 2022-11-08 | 中国科学院国家空间科学中心 | 一种多星自动线性编队和时变基线生成的系统 |
CN113184220B (zh) * | 2021-04-21 | 2021-11-19 | 中国人民解放军63923部队 | 一种地球同步轨道通信卫星的轨道控制方法及装置 |
US11820535B2 (en) * | 2021-09-17 | 2023-11-21 | Maxar Space Llc | Small satellite constellation for worldwide surveillance |
CN115196046B (zh) * | 2022-09-19 | 2022-12-13 | 航天东方红卫星有限公司 | 一种太阳同步轨道卫星超寿运行轨控策略确定方法 |
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US7720604B1 (en) * | 2005-06-01 | 2010-05-18 | Lockheed Martin Corporation | Stationkeeping optimization for inclined elliptical satellite orbit constellations |
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FR2727934A1 (fr) * | 1994-12-08 | 1996-06-14 | Aerospatiale | Satellite geostationnaire stabilise 3-axes a surveillance radar de son espace environnant |
FR2757825B1 (fr) * | 1996-12-31 | 1999-03-26 | Europ Propulsion | Procede et systeme de lancement simultane de satellites sur des orbites non coplanaires en utilisant des orbites tres excentriques et du freinage atmospherique |
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2011
- 2011-10-28 FR FR1103290A patent/FR2982045B1/fr active Active
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- 2012-10-17 ES ES12188770.7T patent/ES2538093T3/es active Active
- 2012-10-17 EP EP12188770.7A patent/EP2586711B1/fr active Active
- 2012-10-18 RU RU2012144413A patent/RU2608186C2/ru active
- 2012-10-19 US US13/656,283 patent/US8783620B2/en active Active
- 2012-10-22 CA CA2792580A patent/CA2792580C/en active Active
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Patent Citations (4)
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JP2004333391A (ja) * | 2003-05-09 | 2004-11-25 | National Institute Of Information & Communication Technology | 静止軌道または静止軌道近傍を通過する軌道を有する物体のスキャン観測方法 |
US7270299B1 (en) * | 2004-03-23 | 2007-09-18 | Northrop Grumman Corporation | Space based change detection using common ground track constellations |
US7720604B1 (en) * | 2005-06-01 | 2010-05-18 | Lockheed Martin Corporation | Stationkeeping optimization for inclined elliptical satellite orbit constellations |
US20080027595A1 (en) * | 2006-07-26 | 2008-01-31 | Fowler Harmon C | Optimizing initial inclinations and RAANs of a satellite constellation |
Also Published As
Publication number | Publication date |
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FR2982045A1 (fr) | 2013-05-03 |
EP2586711B1 (fr) | 2015-03-04 |
US8783620B2 (en) | 2014-07-22 |
RU2608186C2 (ru) | 2017-01-17 |
FR2982045B1 (fr) | 2013-12-27 |
RU2012144413A (ru) | 2014-04-27 |
CA2792580C (en) | 2019-01-15 |
ES2538093T3 (es) | 2015-06-17 |
US20130105632A1 (en) | 2013-05-02 |
DK2586711T3 (en) | 2015-06-01 |
CA2792580A1 (en) | 2013-04-28 |
EP2586711A1 (fr) | 2013-05-01 |
JP6199021B2 (ja) | 2017-09-20 |
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