DE69914205D1 - Drallregelungseinheit für raumfahrzeuglageregelung - Google Patents

Drallregelungseinheit für raumfahrzeuglageregelung

Info

Publication number
DE69914205D1
DE69914205D1 DE69914205T DE69914205T DE69914205D1 DE 69914205 D1 DE69914205 D1 DE 69914205D1 DE 69914205 T DE69914205 T DE 69914205T DE 69914205 T DE69914205 T DE 69914205T DE 69914205 D1 DE69914205 D1 DE 69914205D1
Authority
DE
Germany
Prior art keywords
vehicle position
space vehicle
control unit
swirl
position control
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
Application number
DE69914205T
Other languages
English (en)
Other versions
DE69914205T2 (de
Inventor
P Davis
T Hyde
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honeywell Inc
Original Assignee
Honeywell Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Honeywell Inc filed Critical Honeywell Inc
Publication of DE69914205D1 publication Critical patent/DE69914205D1/de
Application granted granted Critical
Publication of DE69914205T2 publication Critical patent/DE69914205T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B64G1/28—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

Landscapes

  • 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)
DE69914205T 1998-08-26 1999-08-05 Momentensteuereinheit für raumfahrzeuglagesteuerung Expired - Lifetime DE69914205T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09/139,989 US6340137B1 (en) 1998-08-26 1998-08-26 Moment control unit for spacecraft attitude control
US139989 1998-08-26
PCT/US1999/017764 WO2000012269A2 (en) 1998-08-26 1999-08-05 Moment control unit for spacecraft attitude control

Publications (2)

Publication Number Publication Date
DE69914205D1 true DE69914205D1 (de) 2004-02-19
DE69914205T2 DE69914205T2 (de) 2004-11-25

Family

ID=22489219

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69914205T Expired - Lifetime DE69914205T2 (de) 1998-08-26 1999-08-05 Momentensteuereinheit für raumfahrzeuglagesteuerung

Country Status (5)

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

Families Citing this family (19)

* 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
WO2006004581A2 (en) * 2004-04-06 2006-01-12 University Of North Texas 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

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
JPH03501526A (ja) * 1988-05-27 1991-04-04 ハネウエル・インコーポレーテツド スキユー軸慣性センサ組立体
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
US6022005A (en) * 1996-09-27 2000-02-08 Trw Inc. Semi-active vibration isolator and fine positioning mount
US5820078A (en) * 1996-09-27 1998-10-13 Hughes Electronics Corporation Control motion gyro with vibration isolation
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
EP1107852A2 (de) 2001-06-20
JP4266520B2 (ja) 2009-05-20
US6340137B1 (en) 2002-01-22
WO2000012269A3 (en) 2000-06-02
JP2002523291A (ja) 2002-07-30
WO2000012269A2 (en) 2000-03-09
EP1107852B1 (de) 2004-01-14
DE69914205T2 (de) 2004-11-25

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Legal Events

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