GB1130314A - Improvements in vibrating string gyroscopes - Google Patents
Improvements in vibrating string gyroscopesInfo
- Publication number
- GB1130314A GB1130314A GB644266A GB644266A GB1130314A GB 1130314 A GB1130314 A GB 1130314A GB 644266 A GB644266 A GB 644266A GB 644266 A GB644266 A GB 644266A GB 1130314 A GB1130314 A GB 1130314A
- Authority
- GB
- United Kingdom
- Prior art keywords
- string
- axis
- frequency
- plane
- inductor
- 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
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
- G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
- G01C19/5635—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using vibrating wires or strings
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Gyroscopes (AREA)
Abstract
1,130,314. Vibrating string gyros. CSF COMPAGNIE GENERALE DE TELEGRAPHIE SANS FIL. Feb.14, 1966, No.6442/66. Headings G1C and G1N. A system for measuring an angular velocity component about an axis Oz comprises a frame 2, a conductive vibrating string stitched on the frame along the axis Oz, the string being vibrated by supplying to it an alternating current of a frequency f 1 which is one of the resonant frequencies of the string e. g. that corresponding to one wavelength as shown, and by the provision of a D.C. inductor 3 providing a magnetic field along the axis Oy, an A. C. inductor 4 providing an alternating magnetic field along the axis Ox of a frequency f 2 less than f 1 whereby an amplitude modulated signal is induced in the string having a modulation depth which is a function of the sine of the angle of inclination of the plane of vibration of the string to the reference plane xOz caused by the angular velocity component to be measured, and modulation depth measuring means connected across the string, this means comprising a reactance circuit 6, through the two branches of which flow currents i 12 and i 21 corresponding respectively to the components f 1 +f 2 and f 1 -f 2 of the amplitude modulation so that the current flowing through an ammeter 7 connected in series with the circuit 6, deviates in proportion with the rotation of the plane of vibration of the string about the axis Oz. The A. C. current of frequency f 1 is derived from a source which supplies the energy necessary to keep the string in oscillation, e.g. an amplifier with feedback.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR6483A FR1434247A (en) | 1965-02-22 | 1965-02-22 | Improvements to vibrating gyrometers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1130314A true GB1130314A (en) | 1968-10-16 |
Family
ID=8571541
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB644266A Expired GB1130314A (en) | 1965-02-22 | 1966-02-14 | Improvements in vibrating string gyroscopes |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1258163B (en) |
FR (1) | FR1434247A (en) |
GB (1) | GB1130314A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3515003A (en) * | 1966-07-25 | 1970-06-02 | Honeywell Inc | Vibrating wire angular rate sensor |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR955301A (en) * | 1950-01-14 | |||
FR1322871A (en) * | 1962-02-06 | 1963-04-05 | North American Aviation Inc | Stable reference device including gyroscopic device |
FR1380612A (en) * | 1963-10-14 | 1964-12-04 | North American Aviation Inc | Gyroscopic apparatus |
-
1965
- 1965-02-22 FR FR6483A patent/FR1434247A/en not_active Expired
-
1966
- 1966-02-14 GB GB644266A patent/GB1130314A/en not_active Expired
- 1966-02-21 DE DE1966C0038285 patent/DE1258163B/en active Pending
Also Published As
Publication number | Publication date |
---|---|
FR1434247A (en) | 1966-04-08 |
DE1258163B (en) | 1968-01-04 |
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