DE69630989D1 - Universelles Lageregelungssystem für Raumfahrzeug - Google Patents

Universelles Lageregelungssystem für Raumfahrzeug

Info

Publication number
DE69630989D1
DE69630989D1 DE69630989T DE69630989T DE69630989D1 DE 69630989 D1 DE69630989 D1 DE 69630989D1 DE 69630989 T DE69630989 T DE 69630989T DE 69630989 T DE69630989 T DE 69630989T DE 69630989 D1 DE69630989 D1 DE 69630989D1
Authority
DE
Germany
Prior art keywords
spacecraft
control system
attitude control
universal
universal attitude
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
DE69630989T
Other languages
English (en)
Other versions
DE69630989T2 (de
Inventor
John W Smay
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.)
DirecTV Group Inc
Original Assignee
Hughes Electronics Corp
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 Hughes Electronics Corp filed Critical Hughes Electronics Corp
Publication of DE69630989D1 publication Critical patent/DE69630989D1/de
Application granted granted Critical
Publication of DE69630989T2 publication Critical patent/DE69630989T2/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
    • B64G1/285—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
    • B64G1/244—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
    • B64G1/281—Spin-stabilised spacecraft
    • 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)

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)
DE69630989T 1995-05-15 1996-05-04 Universelles Lagerregelungssystem für Raumfahrzeug Expired - Lifetime DE69630989T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/441,359 US5692707A (en) 1995-05-15 1995-05-15 Universal spacecraft attitude steering control system
US441359 1995-05-15

Publications (2)

Publication Number Publication Date
DE69630989D1 true DE69630989D1 (de) 2004-01-22
DE69630989T2 DE69630989T2 (de) 2004-10-28

Family

ID=23752573

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69630989T Expired - Lifetime DE69630989T2 (de) 1995-05-15 1996-05-04 Universelles Lagerregelungssystem für Raumfahrzeug

Country Status (3)

Country Link
US (1) US5692707A (de)
EP (1) EP0743249B1 (de)
DE (1) DE69630989T2 (de)

Families Citing this family (35)

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US5984236A (en) * 1995-12-22 1999-11-16 Keitel; Keith F. Momentum unloading using gimbaled thrusters
US5875676A (en) * 1997-09-02 1999-03-02 Honeywell Inc. Non colocated rate sensing for control moment gyroscopes
US6154691A (en) * 1997-09-02 2000-11-28 Honeywell International Inc. Orienting a satellite with controlled momentum gyros
JP3518362B2 (ja) * 1998-01-06 2004-04-12 日産自動車株式会社 車両のピッチ角演算装置
US6089508A (en) * 1998-03-02 2000-07-18 Hughes Electronics Corporation Autonomous spacecraft safing with reaction wheels
US6039290A (en) * 1998-03-16 2000-03-21 Honeywell Inc. Robust singularity avoidance in satellite attitude control
US6131056A (en) * 1998-03-16 2000-10-10 Honeywell International Inc. Continuous attitude control that avoids CMG array singularities
FR2786283B1 (fr) * 1998-11-19 2001-01-26 Matra Marconi Space France Procede et dispositif de pilotage de l'attitude d'un satellite
US6283416B1 (en) * 1999-06-21 2001-09-04 Aero Astro, Inc. Spacecraft kernel
EP1076005B1 (de) * 1999-08-13 2007-01-03 Hughes Electronics Corporation Umlaufbahnsteuerung eines Raumfahrzeuges bei Rückmeldung der Lage der Umlaufbahn
US6311931B1 (en) * 1999-12-17 2001-11-06 The Boeing Company Bi-directional momentum bias spacecraft attitude control
US6454218B1 (en) * 2000-02-28 2002-09-24 Quoin International, Inc. Integrated system for providing 3-axis attitude-control, energy-storage, and electrical power
US6732977B1 (en) 2002-02-11 2004-05-11 Lockheed Martin Corporation System for on-orbit correction of spacecraft payload pointing errors
US6695263B1 (en) 2002-02-12 2004-02-24 Lockheed Martin Corporation System for geosynchronous spacecraft rapid earth reacquisition
US7051980B2 (en) * 2002-02-26 2006-05-30 Lockheed Martin Corporation Efficient orbit sparing system for space vehicle constellations
US6891498B2 (en) 2002-03-28 2005-05-10 Honeywell International Inc. Inertial reference system for a spacecraft
US6702234B1 (en) * 2002-03-29 2004-03-09 Lockheed Martin Corporation Fault tolerant attitude control system for zero momentum spacecraft
US6682019B2 (en) 2002-04-04 2004-01-27 Honeywell International Inc. Minimum energy wheel configurations for energy storage and attitude control
US6648274B1 (en) 2002-04-12 2003-11-18 David A. Bailey Virtual reaction wheel array
GB2391732B (en) * 2002-05-16 2005-09-07 Furuno Electric Co Attitude sensing apparatus for determining the attitude of a mobile unit
US6523785B1 (en) * 2002-07-02 2003-02-25 Michael Ross Hennigan Reaction wheel desaturation apparatus
US6679457B1 (en) * 2003-01-13 2004-01-20 Honeywell International Inc. Reaction wheel system with vernier control rotor
US7078880B2 (en) * 2003-08-15 2006-07-18 Honeywell International, Inc. Energy storage flywheel voltage regulation and load sharing system and method
US6945500B2 (en) * 2003-08-15 2005-09-20 Skycorp, Inc. Apparatus for a geosynchronous life extension spacecraft
US7364120B2 (en) * 2004-08-26 2008-04-29 Honeywell International, Inc. Quantized control-moment gyroscope array
US20060163434A1 (en) * 2005-01-27 2006-07-27 Honeywell International Inc., Law Dept. Spacecraft for interplanetary/lunar travel
US7835826B1 (en) 2005-12-13 2010-11-16 Lockheed Martin Corporation Attitude determination system for yaw-steering spacecraft
US20080297120A1 (en) * 2006-12-12 2008-12-04 Honeywell International, Inc. Electronically redundant spacecraft power and attitude control system
US20090039202A1 (en) * 2007-02-07 2009-02-12 Keita Ogo Attitude Change Control Method, Attitude Change Control System, Attitude Change Control Program and Program Recording Medium
JP4463287B2 (ja) * 2007-02-07 2010-05-19 Ｎｅｃ東芝スペースシステム株式会社 姿勢変更制御方法、姿勢変更制御システム、姿勢変更制御プログラムおよびプログラム記録媒体
US8352101B2 (en) * 2009-12-22 2013-01-08 The Boeing Company Algorithm for simultaneous attitude maneuver and momentum dumping
US9551994B2 (en) 2015-06-15 2017-01-24 The Boeing Company System and method for vehicle attitude control
JP6373496B2 (ja) * 2015-06-22 2018-08-15 三菱電機株式会社 宇宙機の姿勢制御装置およびｃｍｇのジンバル角演算方法
IT201900019322A1 (it) * 2019-10-18 2021-04-18 Thales Alenia Space Italia Spa Con Unico Socio Assistenza end-to-end in orbita
CN113156987B (zh) * 2021-04-15 2022-05-31 哈尔滨工业大学 结合双框架剪式力矩陀螺和飞轮的航天器执行机构及其控制方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1338483A (fr) * 1962-08-09 1963-09-27 Snecma Perfectionnements aux procédés et dispositifs de stabilisation d'engins spatiaux à volants d'inertie
US3741500A (en) * 1971-04-21 1973-06-26 Sperry Rand Corp A cmg fine attitude control system
US3999729A (en) * 1975-03-20 1976-12-28 Rca Corporation Backup wheel for a three axis reaction wheel spacecraft
US4735382A (en) * 1983-10-28 1988-04-05 The Boeing Company Space craft cellular energy generating and storage device
US4723735A (en) * 1984-12-28 1988-02-09 The Charles Stark Draper Laboratory, Inc. Energy storage attitude control and reference system
DE3644439A1 (de) * 1986-12-24 1988-07-14 Pietzsch Ibp Gmbh Vorrichtung zum richtungspositionieren eines satelliten im weltraum
FR2642552B1 (de) * 1989-01-31 1991-05-24 Europ Propulsion
EP0392130A1 (de) * 1989-04-11 1990-10-17 CONTRAVES ITALIANA S.p.A. Lagekontrolle-Aktuator, insbesondere für ein Raumfahrzeug
US5112012A (en) * 1989-10-26 1992-05-12 Yuan Mark S Tilting momentum wheel for spacecraft
US5261631A (en) * 1991-06-24 1993-11-16 Hughes Aircraft Company Momentum wheel platform steering system and method
WO1994010036A1 (de) * 1992-10-27 1994-05-11 Teldix Gmbh Einrichtung zum schwenken eines flugkörpers, mit zwei kreiseln
US5315158A (en) * 1993-05-17 1994-05-24 Danielson Arnold O Integrated roll control and power supply system and method

Also Published As

Publication number Publication date
DE69630989T2 (de) 2004-10-28
US5692707A (en) 1997-12-02
EP0743249A1 (de) 1996-11-20
EP0743249B1 (de) 2003-12-10

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: WITTE, WELLER & PARTNER, 70178 STUTTGART