JP4266520B2 - 飛行船姿勢制御用のモーメント制御装置 - Google Patents

飛行船姿勢制御用のモーメント制御装置 Download PDF

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Publication number
JP4266520B2
JP4266520B2 JP2000567353A JP2000567353A JP4266520B2 JP 4266520 B2 JP4266520 B2 JP 4266520B2 JP 2000567353 A JP2000567353 A JP 2000567353A JP 2000567353 A JP2000567353 A JP 2000567353A JP 4266520 B2 JP4266520 B2 JP 4266520B2
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Prior art keywords
moment
control
airship
control device
struts
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Expired - Fee Related
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JP2000567353A
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Japanese (ja)
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JP2002523291A (ja
JP2002523291A5 (enExample
Inventor
デイビス，ローレンス．ピー．
ハイド，トリスタム．テイー．
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Honeywell International Inc
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Honeywell International Inc
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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
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • 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
    • B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
    • 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
    • B64G1/285—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum wheels
    • 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors

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  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Vibration Prevention Devices (AREA)
  • Gyroscopes (AREA)
JP2000567353A 1998-08-26 1999-08-05 飛行船姿勢制御用のモーメント制御装置 Expired - Fee Related JP4266520B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09/139,989 1998-08-26
US09/139,989 US6340137B1 (en) 1998-08-26 1998-08-26 Moment control unit for spacecraft attitude control
PCT/US1999/017764 WO2000012269A2 (en) 1998-08-26 1999-08-05 Moment control unit for spacecraft attitude control

Publications (3)

Publication Number Publication Date
JP2002523291A JP2002523291A (ja) 2002-07-30
JP2002523291A5 JP2002523291A5 (enExample) 2006-08-17
JP4266520B2 true JP4266520B2 (ja) 2009-05-20

Family

ID=22489219

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2000567353A Expired - Fee Related JP4266520B2 (ja) 1998-08-26 1999-08-05 飛行船姿勢制御用のモーメント制御装置

Country Status (5)

Country Link
US (1) US6340137B1 (enExample)
EP (1) EP1107852B1 (enExample)
JP (1) JP4266520B2 (enExample)
DE (1) DE69914205T2 (enExample)
WO (1) WO2000012269A2 (enExample)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6550721B2 (en) * 2000-03-09 2003-04-22 The Boeing Company Safing mode for high momentum states in body stabilized spacecraft
US6772978B2 (en) * 2002-02-22 2004-08-10 Honeywell International Inc. Dynamic unbalance compensation system and method
US7121159B2 (en) * 2002-03-01 2006-10-17 Ganid Productions, Llc Apparatus and method for gyroscopic propulsion
US6891498B2 (en) * 2002-03-28 2005-05-10 Honeywell International Inc. Inertial reference system for a spacecraft
US6648274B1 (en) * 2002-04-12 2003-11-18 David A. Bailey Virtual reaction wheel array
US20060032985A1 (en) * 2004-04-06 2006-02-16 Monty Smith Clutch driven reaction wheel steering unit
US7185855B2 (en) * 2004-04-30 2007-03-06 Honeywell International, Inc. Method and system for steering a momentum control system
US7185848B2 (en) * 2004-06-21 2007-03-06 Ltas Holdings, Llc Mass transfer system for stabilizing an airship and other vehicles subject to pitch and roll moments
US7014150B2 (en) * 2004-07-30 2006-03-21 Honeywell International Inc. Method and system for optimizing torque in a CMG array
NL1031263C2 (nl) * 2006-03-01 2007-09-04 Univ Delft Tech Vaartuig, bewegingsplatform, werkwijze voor het compenseren voor bewegingen van een vaartuig en gebruik van een Stewart platform.
US20070284502A1 (en) * 2006-06-13 2007-12-13 Nikon Corporation Hexapod kinematic mountings for optical elements, and optical systems comprising same
US8020809B2 (en) * 2007-04-18 2011-09-20 Ithaco Space Systems, Inc. Direct torque actuator control for control moment gyroscope
FR2924095B1 (fr) * 2007-11-22 2010-02-12 Astrium Sas Actionneur a transfert de moment cinetique pour le controle d'attitude d'un engin spatial
US8312782B2 (en) * 2009-06-18 2012-11-20 Honeywell International Inc. Control moment gyroscope based momentum control systems in small satellites
US20190120623A1 (en) * 2013-03-15 2019-04-25 Mario F. McGuinness Gyroscopic balance unit, 300. and precessional propulsion method
CN106005483B (zh) * 2016-07-06 2018-07-24 西北工业大学 一种模块化手机星的主动姿态控制方法
CN110502024B (zh) * 2019-07-23 2020-10-20 北京控制工程研究所 一种基于空间并联机构的准万向姿态执行机构
CN110712767B (zh) * 2019-10-29 2021-07-30 上海航天控制技术研究所 一种五棱锥构型控制力矩陀螺群自主重构方法
CN110641739B (zh) * 2019-11-09 2024-07-09 深圳市临近空间科技开发有限公司 一种多维度旋转轴连接装置
CN120039426B (zh) * 2025-02-25 2025-12-02 中国科学院微小卫星创新研究院 一种应用于高机动微纳卫星的混合控制构型方法

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3439548A (en) * 1966-01-28 1969-04-22 Tibor Horvath Torque generator
US3452948A (en) * 1967-01-03 1969-07-01 Garrett Corp System and method for free body stabilization and orientation
US3493194A (en) * 1967-07-27 1970-02-03 Nasa Spacecraft experiment pointing and attitude control system
US3741500A (en) * 1971-04-21 1973-06-26 Sperry Rand Corp A cmg fine attitude control system
US3915416A (en) * 1973-08-01 1975-10-28 Nasa Annular momentum control device used for stabilization of space vehicles and the like
US4012018A (en) * 1973-10-04 1977-03-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration All sky pointing attitude control system
US3999729A (en) * 1975-03-20 1976-12-28 Rca Corporation Backup wheel for a three axis reaction wheel spacecraft
US4071211A (en) * 1976-09-23 1978-01-31 Rca Corporation Momentum biased active three-axis satellite attitude control system
US4230294A (en) * 1979-07-23 1980-10-28 Rca Corporation Closed loop roll control for momentum biased satellites
US4375878A (en) * 1980-10-28 1983-03-08 Lockheed Missiles & Space Company, Inc. Space satellite with agile payload orientation system
US4662178A (en) * 1982-01-29 1987-05-05 Rasmusson James K Self contained rotator apparatus
US4723735A (en) * 1984-12-28 1988-02-09 The Charles Stark Draper Laboratory, Inc. Energy storage attitude control and reference system
DE3523160A1 (de) * 1985-06-28 1987-01-08 Peter Dr Kuemmel Kaskadenschubpraezessor
US4825716A (en) * 1987-11-13 1989-05-02 Honeywell, Inc. Single gimbal control moment gyroscope skewed array mounting arrangement
EP0381726A4 (en) * 1988-05-27 1992-08-19 Honeywell Inc. Skewed axis inertial sensor assembly
US5058835A (en) * 1990-06-11 1991-10-22 General Electric Company Wheel speed management control system for spacecraft
FR2670746B1 (fr) * 1990-12-21 1993-04-16 Aerospatiale Systeme de controle d'attitude pour satellite 3-axes,; notamment pour satellite d'observation.
US5305981A (en) * 1991-10-31 1994-04-26 Honeywell Inc. Multiaxis vibration isolation system
US5820079A (en) * 1994-04-05 1998-10-13 Hughes Electronics Mechanism for mounting and actuating a momentum wheel with high vibration isolation
US5476239A (en) * 1994-04-19 1995-12-19 The United States Of America As Represented By The Secretary Of The Navy Gyro platform assembly with a spinning vehicle
US5611505A (en) * 1994-11-18 1997-03-18 Hughes Electronics Spacecraft energy storage, attitude steering and momentum management system
US5820078A (en) * 1996-09-27 1998-10-13 Hughes Electronics Corporation Control motion gyro with vibration isolation
US6022005A (en) * 1996-09-27 2000-02-08 Trw Inc. Semi-active vibration isolator and fine positioning mount
US5918865A (en) 1997-01-29 1999-07-06 Honeywell Inc. Load isolator apparatus
US6089508A (en) * 1998-03-02 2000-07-18 Hughes Electronics Corporation Autonomous spacecraft safing with reaction wheels

Also Published As

Publication number Publication date
JP2002523291A (ja) 2002-07-30
WO2000012269A2 (en) 2000-03-09
DE69914205T2 (de) 2004-11-25
EP1107852A2 (en) 2001-06-20
US6340137B1 (en) 2002-01-22
WO2000012269A3 (en) 2000-06-02
EP1107852B1 (en) 2004-01-14
DE69914205D1 (de) 2004-02-19

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