GB8824889D0 - Dynamically tuned gyroscopes - Google Patents

Dynamically tuned gyroscopes

Info

Publication number
GB8824889D0
GB8824889D0 GB888824889A GB8824889A GB8824889D0 GB 8824889 D0 GB8824889 D0 GB 8824889D0 GB 888824889 A GB888824889 A GB 888824889A GB 8824889 A GB8824889 A GB 8824889A GB 8824889 D0 GB8824889 D0 GB 8824889D0
Authority
GB
United Kingdom
Prior art keywords
dynamically tuned
tuned gyroscopes
gyroscopes
dynamically
tuned
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.)
Withdrawn
Application number
GB888824889A
Other versions
GB2224119A (en
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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Priority to GB8824889A priority Critical patent/GB2224119A/en
Publication of GB8824889D0 publication Critical patent/GB8824889D0/en
Publication of GB2224119A publication Critical patent/GB2224119A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02—Rotary gyroscopes
    • G01C19/04—Details
    • G01C19/28—Pick-offs, i.e. devices for taking-off an indication of the displacement of the rotor axis
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02—Rotary gyroscopes
    • G01C19/04—Details
    • G01C19/30—Erection devices, i.e. devices for restoring rotor axis to a desired position

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Gyroscopes (AREA)
GB8824889A 1988-10-24 1988-10-24 Dynamically tuned gyroscopes Withdrawn GB2224119A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8824889A GB2224119A (en) 1988-10-24 1988-10-24 Dynamically tuned gyroscopes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8824889A GB2224119A (en) 1988-10-24 1988-10-24 Dynamically tuned gyroscopes

Publications (2)

Publication Number Publication Date
GB8824889D0 true GB8824889D0 (en) 1989-04-19
GB2224119A GB2224119A (en) 1990-04-25

Family

ID=10645705

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8824889A Withdrawn GB2224119A (en) 1988-10-24 1988-10-24 Dynamically tuned gyroscopes

Country Status (1)

Country Link
GB (1) GB2224119A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5321986A (en) * 1992-08-21 1994-06-21 Alliedsignal Inc. Polar loop implementation for a two degree of freedom gyro
US6705174B2 (en) * 2001-03-28 2004-03-16 Ganid Productions, Llc Apparatus and method for gyroscopic propulsion
US7121159B2 (en) 2002-03-01 2006-10-17 Ganid Productions, Llc Apparatus and method for gyroscopic propulsion

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3490297A (en) * 1966-03-23 1970-01-20 Martin Marietta Corp Dual-rotor inertial sensor
US3702569A (en) * 1970-11-19 1972-11-14 Singer Co System for eliminating gyro on-off drift effects
US4464943A (en) * 1982-06-14 1984-08-14 Hughes Aircraft Company Seeker gyroscope having reduced cross-coupling between rotor spin and precession

Also Published As

Publication number Publication date
GB2224119A (en) 1990-04-25

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)