DE2523056C2 - Redundantes Trägheitssystem - Google Patents

Redundantes Trägheitssystem

Info

Publication number
DE2523056C2
DE2523056C2 DE2523056A DE2523056A DE2523056C2 DE 2523056 C2 DE2523056 C2 DE 2523056C2 DE 2523056 A DE2523056 A DE 2523056A DE 2523056 A DE2523056 A DE 2523056A DE 2523056 C2 DE2523056 C2 DE 2523056C2
Authority
DE
Germany
Prior art keywords
platform
power supply
gyro
assembly
dodecahedron
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
Application number
DE2523056A
Other languages
German (de)
English (en)
Other versions
DE2523056A1 (de
Inventor
Michael New Milford N.J. Epstein
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.)
Bendix Corp
Original Assignee
Bendix 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 Bendix Corp filed Critical Bendix Corp
Publication of DE2523056A1 publication Critical patent/DE2523056A1/de
Application granted granted Critical
Publication of DE2523056C2 publication Critical patent/DE2523056C2/de
Expired legal-status Critical Current

Links

Classifications

    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/12—Gyroscopes
    • Y10T74/1221—Multiple gyroscopes

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Navigation (AREA)
  • Gyroscopes (AREA)
DE2523056A 1974-06-17 1975-05-24 Redundantes Trägheitssystem Expired DE2523056C2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/480,182 US4020702A (en) 1974-06-17 1974-06-17 Redundant inertial measurement system configuration

Publications (2)

Publication Number Publication Date
DE2523056A1 DE2523056A1 (de) 1976-01-02
DE2523056C2 true DE2523056C2 (de) 1984-01-12

Family

ID=23906968

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2523056A Expired DE2523056C2 (de) 1974-06-17 1975-05-24 Redundantes Trägheitssystem

Country Status (6)

Country Link
US (1) US4020702A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JPS5917762B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE2523056C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2274893A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
GB (1) GB1467559A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
IT (1) IT1039034B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4083117A (en) * 1976-09-24 1978-04-11 Sperry-Sun, Inc. All angle borehole tool
US4212443A (en) * 1978-05-18 1980-07-15 Sperry Corporation Strapped down attitude and heading reference system for aircraft employing skewed axis two-degree-of-freedom rate gyros
FR2431116A1 (fr) * 1978-07-11 1980-02-08 Matra Perfectionnements aux centrales inertielles redondantes pour vehicule spatial
JPS57194307A (en) * 1981-05-26 1982-11-29 Natl Aerospace Lab Three axis orthogonal type inertia reference device
FR2578048B1 (fr) * 1985-02-26 1987-03-20 Applic Gles Electri Meca Installations redondantes de capteurs, pour le controle du pilotage, de l'attitude ou de la navigation de vehicules
DE3600763A1 (de) * 1986-01-14 1987-07-16 Bodenseewerk Geraetetech Inertialsensoranlage fuer navigation und flugfuehrung
DE3634023A1 (de) * 1986-10-07 1988-04-21 Bodenseewerk Geraetetech Integriertes, redundantes referenzsystem fuer die flugregelung und zur erzeugung von kurs- und lageinformationen
DE3702022A1 (de) * 1987-01-24 1988-08-04 Bodenseewerk Geraetetech Traegheitssensoranordnung
EP0381726A4 (en) * 1988-05-27 1992-08-19 Honeywell Inc. Skewed axis inertial sensor assembly
US5297052A (en) * 1989-10-16 1994-03-22 The Boeing Company Integrated fault-tolerant air data inertial reference system
US5363700A (en) * 1992-11-17 1994-11-15 Honeywell Inc. Skewed axis inertial sensor assembly
US6594582B1 (en) * 1999-05-14 2003-07-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration GPS compound eye attitude and navigation sensor and method
CN103389085B (zh) * 2013-07-25 2016-12-28 北京航空航天大学 一种六冗余型光纤陀螺imu台体
CN103389089B (zh) * 2013-07-25 2016-03-16 北京航空航天大学 一种六冗余型光纤捷联惯性导航系统
US10473464B2 (en) * 2018-01-17 2019-11-12 Cubic Corporation Cuboid inertial measurement unit
CN109144091A (zh) * 2018-11-06 2019-01-04 广州极飞科技有限公司 一种飞行控制器及无人飞行器

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3282119A (en) * 1963-09-23 1966-11-01 Bendix Corp Means for effecting initial alignment of a stable platform
US3563662A (en) * 1966-06-13 1971-02-16 Sperry Rand Corp Apparatus for sensing movement about a plurality of axes
US3489004A (en) * 1966-07-21 1970-01-13 Honeywell Inc Navigational reference device
US3477298A (en) * 1966-08-17 1969-11-11 Ambac Ind Gyroscopic apparatus and systems
US3918309A (en) * 1972-03-31 1975-11-11 Bendix Corp Redundant inertial measurement system with improved failure-detection capability

Also Published As

Publication number Publication date
FR2274893A1 (fr) 1976-01-09
JPS513666A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1976-01-13
GB1467559A (en) 1977-03-16
IT1039034B (it) 1979-12-10
DE2523056A1 (de) 1976-01-02
FR2274893B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1977-07-08
US4020702A (en) 1977-05-03
JPS5917762B2 (ja) 1984-04-23

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Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee