DE60310268D1 - Momentumsteuersystem und -verfahren - Google Patents

Momentumsteuersystem und -verfahren

Info

Publication number
DE60310268D1
DE60310268D1 DE60310268T DE60310268T DE60310268D1 DE 60310268 D1 DE60310268 D1 DE 60310268D1 DE 60310268 T DE60310268 T DE 60310268T DE 60310268 T DE60310268 T DE 60310268T DE 60310268 D1 DE60310268 D1 DE 60310268D1
Authority
DE
Germany
Prior art keywords
control system
momentum control
momentum
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
DE60310268T
Other languages
English (en)
Other versions
DE60310268T2 (de
Inventor
Alan Peck
Tupper 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 International Inc
Original Assignee
Honeywell International 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 International Inc filed Critical Honeywell International Inc
Publication of DE60310268D1 publication Critical patent/DE60310268D1/de
Application granted granted Critical
Publication of DE60310268T2 publication Critical patent/DE60310268T2/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
    • B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
DE60310268T 2002-12-30 2003-12-22 Momentumsteuersystem und -verfahren Expired - Lifetime DE60310268T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US10/334,202 US6758444B1 (en) 2002-12-30 2002-12-30 Momentum control system and method
US334202 2002-12-30
PCT/US2003/041816 WO2004101360A2 (en) 2002-12-30 2003-12-22 Momentum control system and method

Publications (2)

Publication Number Publication Date
DE60310268D1 true DE60310268D1 (de) 2007-01-18
DE60310268T2 DE60310268T2 (de) 2007-05-31

Family

ID=32594777

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60310268T Expired - Lifetime DE60310268T2 (de) 2002-12-30 2003-12-22 Momentumsteuersystem und -verfahren

Country Status (5)

Country Link
US (1) US6758444B1 (de)
EP (1) EP1583691B1 (de)
AU (1) AU2003304121A1 (de)
DE (1) DE60310268T2 (de)
WO (1) WO2004101360A2 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2957895B1 (fr) 2010-03-29 2013-09-27 Astrium Sas Procede de commande d'un systeme de controle d'attitude et systeme de controle d'attitude d'un vehicule spatial

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1011715A (en) * 1974-03-18 1977-06-07 Asim K. Sen Attitude stabilization and control of dual-spin spacecraft
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
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.
US5335179A (en) * 1992-12-24 1994-08-02 General Electric Co. Unified spacecraft attitude control system with pseudo-complementary paired thrusters
DE59608525D1 (de) * 1995-08-11 2002-01-31 Astrium Gmbh Verfahren zur Lageregelung und Stabilisierung eines Raumfahrzeuges
US5754023A (en) * 1995-10-26 1998-05-19 Cybernet Systems Corporation Gyro-stabilized platforms for force-feedback applications
US5826829A (en) * 1996-07-15 1998-10-27 Space Systems/Loral Inc. Spacecraft control system with a trihedral momentum bias wheel configuration
US5873285A (en) 1997-05-13 1999-02-23 Honeywell Inc. Modular reaction wheel
US6076772A (en) * 1997-12-15 2000-06-20 Hughes Electronics Corporation Methods for controlling spacecraft attitudes without exciting spacecraft resonances
US6089508A (en) * 1998-03-02 2000-07-18 Hughes Electronics Corporation Autonomous spacecraft safing with reaction wheels
US6138953A (en) * 1998-03-02 2000-10-31 Hughes Electronics Corporation Slew rate direction determination for acquisition maneuvers using reaction wheels
FR2786283B1 (fr) * 1998-11-19 2001-01-26 Matra Marconi Space France Procede et dispositif de pilotage de l'attitude d'un satellite

Also Published As

Publication number Publication date
EP1583691A2 (de) 2005-10-12
AU2003304121A1 (en) 2004-12-03
US20040124314A1 (en) 2004-07-01
AU2003304121A8 (en) 2004-12-03
WO2004101360A2 (en) 2004-11-25
US6758444B1 (en) 2004-07-06
EP1583691B1 (de) 2006-12-06
DE60310268T2 (de) 2007-05-31
WO2004101360A3 (en) 2005-01-20

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition