JP5159921B2 - 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 - Google Patents

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 Download PDF

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JP5159921B2
JP5159921B2 JP2011135072A JP2011135072A JP5159921B2 JP 5159921 B2 JP5159921 B2 JP 5159921B2 JP 2011135072 A JP2011135072 A JP 2011135072A JP 2011135072 A JP2011135072 A JP 2011135072A JP 5159921 B2 JP5159921 B2 JP 5159921B2
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force
displacement
magnitude
spacecraft
determining
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JP2012025381A (ja
JP2012025381A5 (enExample
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クリスチャン・チラン
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Mitsubishi Electric Research Laboratories Inc
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Mitsubishi Electric Research Laboratories Inc
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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
    • 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
    • B64G1/244—Spacecraft control systems
    • B64G1/245—Attitude control algorithms for spacecraft attitude control
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • G05D1/104—Simultaneous control of position or course in three dimensions specially adapted for aircraft involving a plurality of aircrafts, e.g. formation flying

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  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Astronomy & Astrophysics (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
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

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

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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

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* 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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US8244417B2 (en) 2012-08-14
JP2012025381A (ja) 2012-02-09
US20120022726A1 (en) 2012-01-26

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