JP2012025381A5 - - Google Patents

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Publication number
JP2012025381A5
JP2012025381A5 JP2011135072A JP2011135072A JP2012025381A5 JP 2012025381 A5 JP2012025381 A5 JP 2012025381A5 JP 2011135072 A JP2011135072 A JP 2011135072A JP 2011135072 A JP2011135072 A JP 2011135072A JP 2012025381 A5 JP2012025381 A5 JP 2012025381A5
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JP
Japan
Prior art keywords
force
displacement
magnitude
determining
spacecraft
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JP2011135072A
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English (en)
Japanese (ja)
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JP2012025381A (ja
JP5159921B2 (ja
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Priority claimed from US12/840,959 external-priority patent/US8244417B2/en
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Publication of JP2012025381A publication Critical patent/JP2012025381A/ja
Publication of JP2012025381A5 publication Critical patent/JP2012025381A5/ja
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Publication of JP5159921B2 publication Critical patent/JP5159921B2/ja
Expired - Fee Related legal-status Critical Current
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JP2011135072A 2010-07-21 2011-06-17 宇宙船の姿勢維持方法、制御モジュールおよび変位補正力の決定方法 Expired - Fee Related JP5159921B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/840,959 US8244417B2 (en) 2010-07-21 2010-07-21 Method for maintaining pose of spacecraft
US12/840,959 2010-07-21

Publications (3)

Publication Number Publication Date
JP2012025381A JP2012025381A (ja) 2012-02-09
JP2012025381A5 true JP2012025381A5 (enExample) 2012-12-06
JP5159921B2 JP5159921B2 (ja) 2013-03-13

Family

ID=45494262

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011135072A Expired - Fee Related JP5159921B2 (ja) 2010-07-21 2011-06-17 宇宙船の姿勢維持方法、制御モジュールおよび変位補正力の決定方法

Country Status (2)

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US (1) US8244417B2 (enExample)
JP (1) JP5159921B2 (enExample)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2983981B1 (fr) * 2011-12-09 2014-08-22 Thales Sa Procede et systeme de commande d'un ensemble d'au moins deux satellites, concus pour fournir un service sur une orbite geostationnaire, rendant ledit service sur une orbite non-geostationnaire
JP6000091B2 (ja) 2012-11-27 2016-09-28 三菱重工業株式会社 軌道姿勢制御装置、軌道姿勢制御方法
JP2014105657A (ja) 2012-11-28 2014-06-09 Mitsubishi Heavy Ind Ltd 軌道姿勢制御装置、軌道姿勢制御方法
JP6008713B2 (ja) * 2012-11-28 2016-10-19 三菱重工業株式会社 軌道姿勢制御装置、軌道姿勢制御方法
CN108614578B (zh) * 2018-05-31 2020-09-18 北京航空航天大学 一种小推力悬浮轨道上航天器编队飞行方法
CN109398764B (zh) * 2018-11-15 2020-08-14 上海航天控制技术研究所 一种远地点点火姿态偏差辨识方法
CN117208230A (zh) * 2023-07-28 2023-12-12 江苏科技大学 一种基于强化学习的航天器姿态预设定时间协同控制方法

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5267167A (en) * 1991-05-10 1993-11-30 Ball Corporation Method and system for formationfinding and formationkeeping in a constellation of satellites
US6205378B1 (en) * 1999-07-29 2001-03-20 Space Systems/Loral, Inc. Adaptive mass expulsion attitude control system

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