DE60300944D1 - Trägheitsreferenzsystem für ein raumfahrzeug - Google Patents

Trägheitsreferenzsystem für ein raumfahrzeug

Info

Publication number
DE60300944D1
DE60300944D1 DE60300944T DE60300944T DE60300944D1 DE 60300944 D1 DE60300944 D1 DE 60300944D1 DE 60300944 T DE60300944 T DE 60300944T DE 60300944 T DE60300944 T DE 60300944T DE 60300944 D1 DE60300944 D1 DE 60300944D1
Authority
DE
Germany
Prior art keywords
reference system
space vehicle
inertia reference
inertia
vehicle
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
DE60300944T
Other languages
English (en)
Other versions
DE60300944T2 (de
Inventor
H Jacobs
E Meffe
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
Application granted granted Critical
Publication of DE60300944D1 publication Critical patent/DE60300944D1/de
Publication of DE60300944T2 publication Critical patent/DE60300944T2/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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/369—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using gyroscopes as attitude sensors
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/166—Mechanical, construction or arrangement details of inertial navigation systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/183—Compensation of inertial measurements, e.g. for temperature effects
    • 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
    • B64G1/286—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)
  • Radar, Positioning & Navigation (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)
DE60300944T 2002-03-28 2003-03-28 Trägheitsreferenzsystem für ein raumfahrzeug Expired - Lifetime DE60300944T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US10/108,306 US6891498B2 (en) 2002-03-28 2002-03-28 Inertial reference system for a spacecraft
US108306 2002-03-28
PCT/US2003/009742 WO2003082673A1 (en) 2002-03-28 2003-03-28 Inertial reference system for a spacecraft

Publications (2)

Publication Number Publication Date
DE60300944D1 true DE60300944D1 (de) 2005-08-04
DE60300944T2 DE60300944T2 (de) 2006-05-11

Family

ID=28673596

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60300944T Expired - Lifetime DE60300944T2 (de) 2002-03-28 2003-03-28 Trägheitsreferenzsystem für ein raumfahrzeug

Country Status (5)

Country Link
US (1) US6891498B2 (de)
EP (1) EP1487700B1 (de)
AU (1) AU2003223395A1 (de)
DE (1) DE60300944T2 (de)
WO (1) WO2003082673A1 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6775599B2 (en) * 2002-07-10 2004-08-10 Honeywell International Inc. Multi-function reaction wheel assemblies for controlling spacecraft attitude
FR2846107B1 (fr) * 2002-10-21 2005-06-24 Cit Alcatel Dispositif de controle d'attitude d'un satellite geostationnaire
US7570468B2 (en) * 2006-07-05 2009-08-04 Atmel Corporation Noise immune RC trigger for ESD protection
US7760476B2 (en) * 2007-06-07 2010-07-20 Atmel Corporation Threshold voltage method and apparatus for ESD protection
US9261419B2 (en) 2014-01-23 2016-02-16 Honeywell International Inc. Modular load structure assembly having internal strain gaged sensing
US20150367968A1 (en) * 2014-06-19 2015-12-24 Honeywell International Inc. Systems and methods for a momentum platform
US9641287B2 (en) 2015-01-13 2017-05-02 Honeywell International Inc. Methods and apparatus for high-integrity data transfer with preemptive blocking
US9739568B2 (en) * 2015-09-10 2017-08-22 The Boeing Company Methods of connecting testing equipment to a missile system
US20180198388A1 (en) * 2017-01-06 2018-07-12 Honeywell International Inc. High efficiency actuator for use in a momentum control device
CN110194284B (zh) * 2019-06-19 2020-08-21 北京千乘探索科技有限公司 一种遥感卫星动量轮隔振支架及其制作方法

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4445376A (en) 1982-03-12 1984-05-01 Technion Research And Development Foundation Ltd. Apparatus and method for measuring specific force and angular rate
US4512192A (en) 1983-09-02 1985-04-23 Sundstrand Data Control, Inc. Two axis angular rate and specific force sensor utilizing vibrating accelerometers
US4723735A (en) 1984-12-28 1988-02-09 The Charles Stark Draper Laboratory, Inc. Energy storage attitude control and reference system
US4732353A (en) 1985-11-07 1988-03-22 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Three axis attitude control system
US4825716A (en) 1987-11-13 1989-05-02 Honeywell, Inc. Single gimbal control moment gyroscope skewed array mounting arrangement
US5386738A (en) 1992-12-22 1995-02-07 Honeywell Inc. Direct torque control moment gyroscope
US5437420A (en) 1993-07-16 1995-08-01 Hughes Aircraft Company High torque double gimbal control moment gyro
US5611505A (en) 1994-11-18 1997-03-18 Hughes Electronics Spacecraft energy storage, attitude steering and momentum management system
US5692707A (en) 1995-05-15 1997-12-02 Hughes Aircraft Company Universal spacecraft attitude steering control system
US6022005A (en) * 1996-09-27 2000-02-08 Trw Inc. Semi-active vibration isolator and fine positioning mount
US5875676A (en) 1997-09-02 1999-03-02 Honeywell Inc. Non colocated rate sensing for control moment gyroscopes
US6128556A (en) 1998-03-16 2000-10-03 Honeywell International Inc. CMG control based on angular momentum to control satellite attitude
US6131056A (en) 1998-03-16 2000-10-10 Honeywell International Inc. Continuous attitude control that avoids CMG array singularities
US6047927A (en) 1998-03-16 2000-04-11 Honeywell Inc. Escaping singularities in a satellite attitude control
US6039290A (en) 1998-03-16 2000-03-21 Honeywell Inc. Robust singularity avoidance in satellite attitude control
US6340137B1 (en) 1998-08-26 2002-01-22 Honeywell International Inc. Moment control unit for spacecraft attitude control
US6135392A (en) 1998-09-29 2000-10-24 Hughes Electronics Corporation Spacecraft attitude control actuator and method
US6182582B1 (en) 1999-06-28 2001-02-06 Honeywell International Inc. Tilt table

Also Published As

Publication number Publication date
DE60300944T2 (de) 2006-05-11
EP1487700A1 (de) 2004-12-22
US6891498B2 (en) 2005-05-10
EP1487700B1 (de) 2005-06-29
US20030192996A1 (en) 2003-10-16
AU2003223395A1 (en) 2003-10-13
WO2003082673A1 (en) 2003-10-09

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition