GB1303237A - - Google Patents
Info
- Publication number
- GB1303237A GB1303237A GB4203971A GB4203971A GB1303237A GB 1303237 A GB1303237 A GB 1303237A GB 4203971 A GB4203971 A GB 4203971A GB 4203971 A GB4203971 A GB 4203971A GB 1303237 A GB1303237 A GB 1303237A
- Authority
- GB
- United Kingdom
- Prior art keywords
- bell
- angular displacement
- vibration
- natural frequency
- capacitive electrode
- 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
- 238000006073 displacement reaction Methods 0.000 abstract 2
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
- G01C19/567—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using the phase shift of a vibration node or antinode
- G01C19/5691—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using the phase shift of a vibration node or antinode of essentially three-dimensional vibrators, e.g. wine glass-type vibrators
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Gyroscopes (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US7706770A | 1970-10-01 | 1970-10-01 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1303237A true GB1303237A (enExample) | 1973-01-17 |
Family
ID=22135883
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB4203971A Expired GB1303237A (enExample) | 1970-10-01 | 1971-09-09 |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3719074A (enExample) |
| CA (1) | CA933378A (enExample) |
| GB (1) | GB1303237A (enExample) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0565384A1 (en) * | 1992-04-10 | 1993-10-13 | British Aerospace Public Limited Company | Single axis rate sensor noise reduction |
| FR2919718A1 (fr) * | 2007-08-03 | 2009-02-06 | Northrop Grumman Guidance & El | Gyroscope a resonateur hemispherique millimetrique a dispositif de force interne. |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3924475A (en) * | 1973-10-23 | 1975-12-09 | Singer Co | Vibrating ring gyro |
| US4157041A (en) * | 1978-05-22 | 1979-06-05 | General Motors Corporation | Sonic vibrating bell gyro |
| US4951508A (en) * | 1983-10-31 | 1990-08-28 | General Motors Corporation | Vibratory rotation sensor |
| US4759220A (en) * | 1986-02-28 | 1988-07-26 | Burdess James S | Angular rate sensors |
| US4793195A (en) * | 1986-10-20 | 1988-12-27 | Northrop Corporation | Vibrating cylinder gyroscope and method |
| US5383362A (en) * | 1993-02-01 | 1995-01-24 | General Motors Corporation | Control for vibratory gyroscope |
| US5850041A (en) * | 1997-03-21 | 1998-12-15 | Litton Systems, Inc. | Vibratory rotation sensor with AC forcing and sensing electronics |
| US5827966A (en) * | 1997-05-29 | 1998-10-27 | Litton Systems, Inc. | Vibratory rotation sensor utilizing linearized flexure measures |
| US6401556B1 (en) | 1999-06-23 | 2002-06-11 | Peter Winston Hamady | Precessional device and method thereof |
| US6629908B2 (en) | 2000-05-09 | 2003-10-07 | Peter Winston Hamady | Precessional apparatus and method thereof |
| FR2816702B1 (fr) * | 2000-11-13 | 2003-01-24 | Sagem | Dispositif de stabilisation de plate-forme autour d'un axe, utilisant un detecteur a resonateur vibrant |
| US20070298942A1 (en) * | 2003-05-02 | 2007-12-27 | Hamady Peter W | Precessional device with secondary portion |
| US7181987B2 (en) * | 2003-05-02 | 2007-02-27 | Peter Winston Hamady | Precessional device and method |
| US20100139373A1 (en) * | 2005-08-19 | 2010-06-10 | Honeywell Internationa Inc. | Mems sensor package |
| US20070056370A1 (en) * | 2005-08-19 | 2007-03-15 | Honeywell International Inc. | Mems sensor package |
| US7296468B2 (en) * | 2005-10-26 | 2007-11-20 | Litton Systems, Inc. | Digital coriolis gyroscope |
| US7251900B2 (en) * | 2005-10-26 | 2007-08-07 | Guy Thomas Varty | Methods and systems utilizing intermediate frequencies to control multiple coriolis gyroscopes |
| US7543496B2 (en) * | 2006-03-27 | 2009-06-09 | Georgia Tech Research Corporation | Capacitive bulk acoustic wave disk gyroscopes |
| US7767484B2 (en) | 2006-05-31 | 2010-08-03 | Georgia Tech Research Corporation | Method for sealing and backside releasing of microelectromechanical systems |
| US8061201B2 (en) | 2007-07-13 | 2011-11-22 | Georgia Tech Research Corporation | Readout method and electronic bandwidth control for a silicon in-plane tuning fork gyroscope |
| FR2937413B1 (fr) * | 2008-10-22 | 2010-11-26 | Sagem Defense Securite | Procede de commande d'un capteur a resonateur vibrant a demarrage rapide |
| WO2011026100A1 (en) | 2009-08-31 | 2011-03-03 | Georgia Tech Research Corporation | Bulk acoustic wave gyroscope with spoked structure |
| US9742373B2 (en) | 2011-10-31 | 2017-08-22 | The Regents Of The University Of Michigan | Method of manufacturing a temperature-compensated micromechanical resonator |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3307409A (en) * | 1959-02-26 | 1967-03-07 | Jr George C Newton | Method of and apparatus for measuring angular motion |
| US3408872A (en) * | 1965-10-14 | 1968-11-05 | Air Force Usa | Circumferential flexure vibrating gyroscope |
-
1970
- 1970-10-01 US US00077067A patent/US3719074A/en not_active Expired - Lifetime
-
1971
- 1971-07-19 CA CA118524A patent/CA933378A/en not_active Expired
- 1971-09-09 GB GB4203971A patent/GB1303237A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0565384A1 (en) * | 1992-04-10 | 1993-10-13 | British Aerospace Public Limited Company | Single axis rate sensor noise reduction |
| US5419194A (en) * | 1992-04-10 | 1995-05-30 | British Aerospace Public Limited Company | Single axis rate sensor noise reduction |
| FR2919718A1 (fr) * | 2007-08-03 | 2009-02-06 | Northrop Grumman Guidance & El | Gyroscope a resonateur hemispherique millimetrique a dispositif de force interne. |
Also Published As
| Publication number | Publication date |
|---|---|
| CA933378A (en) | 1973-09-11 |
| US3719074A (en) | 1973-03-06 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed [section 19, patents act 1949] | ||
| PCNP | Patent ceased through non-payment of renewal fee |