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GB2129554B - Attitude gyro for projectile - Google Patents
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GB2129554B - Attitude gyro for projectile - Google Patents

Attitude gyro for projectile

Info

Publication number
GB2129554B
GB2129554B GB08111112A GB8111112A GB2129554B GB 2129554 B GB2129554 B GB 2129554B GB 08111112 A GB08111112 A GB 08111112A GB 8111112 A GB8111112 A GB 8111112A GB 2129554 B GB2129554 B GB 2129554B
Authority
GB
United Kingdom
Prior art keywords
projectile
attitude gyro
gyro
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
Application number
GB08111112A
Other versions
GB2129554A (en
Inventor
Ernst Gruber
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB2129554A publication Critical patent/GB2129554A/en
Application granted granted Critical
Publication of GB2129554B publication Critical patent/GB2129554B/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02Rotary gyroscopes
    • G01C19/025Gyroscopes functioning for short periods
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02Rotary gyroscopes
    • G01C19/04Details
    • G01C19/16Suspensions; Bearings

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Support Of The Bearing (AREA)
  • Gyroscopes (AREA)
GB08111112A 1980-04-16 1981-04-09 Attitude gyro for projectile Expired GB2129554B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19803014480 DE3014480C1 (en) 1980-04-16 1980-04-16 Acceleration-resistant gyroscope for missiles

Publications (2)

Publication Number Publication Date
GB2129554A GB2129554A (en) 1984-05-16
GB2129554B true GB2129554B (en) 1984-12-05

Family

ID=6100091

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08111112A Expired GB2129554B (en) 1980-04-16 1981-04-09 Attitude gyro for projectile

Country Status (3)

Country Link
DE (1) DE3014480C1 (en)
FR (1) FR2538540A1 (en)
GB (1) GB2129554B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4122285A1 (en) * 1991-07-05 1993-01-07 Bodenseewerk Geraetetech THREE-AXIS LASER CIRCUIT
DE4141312C1 (en) * 1991-12-14 1993-02-25 Deutsche Aerospace Ag, 8000 Muenchen, De
FR2731203B1 (en) * 1995-03-02 1997-05-30 Aerospatiale PNEUMATIC DEVICE FOR LOCKING / UNLOCKING A ROTOR ON A STATOR
WO2019183675A1 (en) * 2018-03-28 2019-10-03 Verton IP Pty Ltd Improved arrangements for rotational apparatus

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB497707A (en) * 1937-06-17 1938-12-19 Sperry Gyroscope Co Ltd Improvements relating to gyroscopic instruments
GB553094A (en) * 1940-04-26 1943-05-07 Sperry Gyroscope Co Inc Improvements in and relating to gyroscopic apparatus
GB745653A (en) * 1953-02-10 1956-02-29 Kelvin & Hughes Ltd Improvements in or relating to gyroscopic apparatus
US3618403A (en) * 1969-03-03 1971-11-09 Singer Co Stop assembly for a gyroscope
US3585866A (en) * 1969-07-01 1971-06-22 Singer General Precision Gyroscope flexure hinge suspension
US3677097A (en) * 1971-03-05 1972-07-18 Sperry Rand Corp Protective stops for a flexure suspended gyroscopic rotor
US4155521A (en) * 1975-12-08 1979-05-22 The Singer Company Cannon launched platform
FR2344000A1 (en) * 1976-03-12 1977-10-07 Realisations Electronique Et Gyroscope for high acceleration missile - has two gimbals remaining caged during run-up of wheel and high acceleration phase of missile

Also Published As

Publication number Publication date
GB2129554A (en) 1984-05-16
FR2538540A1 (en) 1984-06-29
DE3014480C1 (en) 1986-07-17

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee