JP5639685B2 - 自己較正型加速度計 - Google Patents
自己較正型加速度計 Download PDFInfo
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- JP5639685B2 JP5639685B2 JP2013103643A JP2013103643A JP5639685B2 JP 5639685 B2 JP5639685 B2 JP 5639685B2 JP 2013103643 A JP2013103643 A JP 2013103643A JP 2013103643 A JP2013103643 A JP 2013103643A JP 5639685 B2 JP5639685 B2 JP 5639685B2
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P21/00—Testing or calibrating of apparatus or devices covered by the preceding groups
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/08—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/08—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
- G01P2015/0805—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration
- G01P2015/0822—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass
- G01P2015/0825—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass for one single degree of freedom of movement of the mass
- G01P2015/0831—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass for one single degree of freedom of movement of the mass the mass being of the paddle type having the pivot axis between the longitudinal ends of the mass, e.g. see-saw configuration
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Pressure Sensors (AREA)
- Gyroscopes (AREA)
Description
なお、本出願は、本出願と同じ被譲渡人に譲渡されている以下の出願の内容と関連する内容を含む。すなわち、2006年8月7日に出願された“Bias and Quadrature Reduction in Class II Coriolis Vibratory Gyros”と題する米国特許出願第11/499,957号(NGC−279/001039−199)と、2006年8月7日に出願された“Method for Modifying the Location of Nodal Points of a Vibrating Beam”と題する米国特許出願第11/499,956号(NGC−202/001047−199)と、2005年2月11日に出願された“Oscillation of Vibrating Beam in a First Direction for a First Time Period and a Second Direction for a Second Time Period to Sense Angular Rate of the Vibrating Beam”と題するRobert E. Stewartによる米国特許出願第11/057,324号(NGC−0167/000602−199)と、2004年12月13日に出願された"Coplanar Proofmasses Employable To Sense Acceleration Along Three Axes"と題する米国特許出願第11/010,588号(NGC−165/000554−199)と、2006年2月28日に出願された"Self-Calibration For An Inertial Instrument Biases On Real Time Bias Estimator"と題する米国特許出願第11/364,316号(NGC−274/000856−199)と、である。
加速度計の出力は、2006年2月28日に出願された米国特許出願第11/364,316号に記載されたリアルタイムのバイアス評価アルゴリズムを用いたデジタル信号プロセッサにおいて処理される。
また、MEMS3軸平面加速度計も、2004年12月13日に出願された米国特許出願第11/010,588号に記載されている。
パルス幅変調された電荷制御サーボを用いて静電力再平衡化されているプルーフマスは、米国特許第5,142,921号に記載されている。付勢方法は、"Bi-stable Micro Actuator and Optical Switch"と題する米国特許第6,591,027号に記載されている。質量変調の原理は、"High Accuracy Accelerometer"と題する米国特許第4,599,896号に記載されている。
MeasB(i)=Win(i)+/−BiasB
第1及び第2の測定間隔に関しては、次の通りである。
MeasA(1)=Win(1)+BiasA
MeasB(1)=Win(1)+BiasB
MeasA(2)=Win(2)−BiasA
MeasB(2)=Win(2)+BiasB
Claims (6)
- 加速度計バイアスを自己較正する方法であって、
静的条件及び動的条件の両方の下で継続的に加速度バイアスを自己較正して、ノイズ源としての加速度バイアスを削除するステップと、
2つの加速度計それぞれの極性を、各加速度計の感知要素の支持中心線の対向する側に、該感知要素の質量中心の位置を交互に移動させることによって、シーケンシャルに交代させつつ、該2つの加速度計によって連続的かつ同時的に加速度を測定する測定ステップと、
デジタル信号プロセッサにおいて、リアルタイムのバイアス評価アルゴリズムを用いて、2つの加速度計の出力からの測定された加速度を処理して、加速度計のバイスを自己較正するステップと
からなることを特徴とする方法。 - 請求項1記載の方法において、測定ステップは、プルーフマス内にある二次質量を平面内で移動させて、質量中心を左右に移動させるステップを含むことを特徴とする方法。
- 請求項2記載の方法において、測定ステップは、質量中心を、支持中心線の一方の側から他方の側に再配置することにより、入力軸の極性を反転させるステップを含むことを特徴とする方法。
- 請求項2記載の方法において、測定ステップは、加速度下において、感知要素を、質量中心が第1の質量中心位置(CG1)にある場合は支持中心線を中心にして時計回りに、質量中心が第2の質量中心位置(CG2)にある場合は支持中心線を中心にして反時計回りに回転させるステップを含んでいることを特徴とする方法。
- 請求項4記載の方法において、2つの加速度計の極性の変更は、質量中心を、第1の質量中心位置(CG1)及び第2の質量中心位置(CG2)の間で、感知要素の支持中心線(CS)の上下に移動させることにより実行されることを特徴とする方法。
- 請求項5記載の方法において、二次質量は、平面の上下に移動することを特徴とする方法。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/729,007 US7640786B2 (en) | 2007-03-28 | 2007-03-28 | Self-calibrating accelerometer |
US11/729,007 | 2007-03-28 |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2008086549A Division JP5275661B2 (ja) | 2007-03-28 | 2008-03-28 | 自己較正型加速度計 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2013152253A JP2013152253A (ja) | 2013-08-08 |
JP5639685B2 true JP5639685B2 (ja) | 2014-12-10 |
Family
ID=39561777
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2008086549A Expired - Fee Related JP5275661B2 (ja) | 2007-03-28 | 2008-03-28 | 自己較正型加速度計 |
JP2013103643A Expired - Fee Related JP5639685B2 (ja) | 2007-03-28 | 2013-05-16 | 自己較正型加速度計 |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2008086549A Expired - Fee Related JP5275661B2 (ja) | 2007-03-28 | 2008-03-28 | 自己較正型加速度計 |
Country Status (3)
Country | Link |
---|---|
US (1) | US7640786B2 (ja) |
EP (1) | EP1975631B1 (ja) |
JP (2) | JP5275661B2 (ja) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE528404C2 (sv) * | 2004-10-20 | 2006-11-07 | Imego Ab | Sensorarrangemang |
US9062971B2 (en) * | 2008-03-06 | 2015-06-23 | Texas Instruments Incorporated | E-compass, tilt sensor, memory and processor with coarse detilting procedure |
US7980115B2 (en) * | 2008-05-30 | 2011-07-19 | Northrop Grumman Guidance and Electronic Co, Inc. | Self-calibrating laser semiconductor accelerometer |
US20110077891A1 (en) * | 2009-09-25 | 2011-03-31 | Sirf Technology Holdings, Inc. | Accelerometer-only calibration method |
DE102011006427A1 (de) * | 2011-03-30 | 2012-10-04 | Robert Bosch Gmbh | Drehratensensor und Verfahren zur Kalibrierung eines Drehratensensors |
US9229026B2 (en) | 2011-04-13 | 2016-01-05 | Northrop Grumman Guaidance and Electronics Company, Inc. | Accelerometer systems and methods |
US9551728B2 (en) | 2011-05-09 | 2017-01-24 | Ramot At Tel Aviv University Ltd. | Bistable force and/or acceleration sensor |
US8371882B1 (en) * | 2011-08-03 | 2013-02-12 | Tyco Electronics Corporation | Straddle mount connector for a pluggable transceiver module |
US9702897B2 (en) * | 2012-10-08 | 2017-07-11 | Northrop Grumman Systems Corporation | Dynamic self-calibration of an accelerometer system |
US9341646B2 (en) | 2012-12-19 | 2016-05-17 | Northrop Grumman Guidance And Electronics Company, Inc. | Bias reduction in force rebalanced accelerometers |
US10352960B1 (en) * | 2015-10-30 | 2019-07-16 | Garmin International, Inc. | Free mass MEMS accelerometer |
ITUA20162172A1 (it) * | 2016-03-31 | 2017-10-01 | St Microelectronics Srl | Sensore accelerometrico realizzato in tecnologia mems avente elevata accuratezza e ridotta sensibilita' nei confronti della temperatura e dell'invecchiamento |
US11525941B2 (en) | 2018-03-28 | 2022-12-13 | Halliburton Energy Services, Inc. | In-situ calibration of borehole gravimeters |
IT201900017546A1 (it) | 2019-09-30 | 2021-03-30 | St Microelectronics Srl | Dispositivo a pulsante mems resistente all'acqua, dispositivo di ingresso comprendente il dispositivo a pulsante mems e apparecchio elettronico |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3241355A (en) * | 1963-05-31 | 1966-03-22 | Honeywell Inc | Accelerometer calibration means |
US4599896A (en) * | 1983-02-22 | 1986-07-15 | Litton Systems, Inc. | High accuracy accelerometer |
US5142921A (en) | 1990-10-29 | 1992-09-01 | Litton Systems, Inc. | Force balance instrument with electrostatic charge control |
US5886259A (en) * | 1996-04-01 | 1999-03-23 | Alliedsignal Inc. | Axis aligned rate and acceleration sensor |
JP2000338129A (ja) * | 1999-03-19 | 2000-12-08 | Ngk Insulators Ltd | 加速度センサ素子の感度較正方法 |
DE10060091B4 (de) * | 2000-12-02 | 2004-02-05 | Eads Deutschland Gmbh | Mikromechanischer Inertialsensor |
US6591027B2 (en) | 2001-02-27 | 2003-07-08 | Litton Systems, Inc. | Bi-stable micro-actuator and optical switch |
US6701786B2 (en) * | 2002-04-29 | 2004-03-09 | L-3 Communications Corporation | Closed loop analog gyro rate sensor |
EP1711836A1 (en) | 2004-01-07 | 2006-10-18 | Northrop Grumman Corporation | Coplanar proofmasses employable to sense acceleration along three axes |
US7073380B2 (en) * | 2004-02-17 | 2006-07-11 | Honeywell International, Inc. | Pyramid socket suspension |
US7066004B1 (en) * | 2004-09-02 | 2006-06-27 | Sandia Corporation | Inertial measurement unit using rotatable MEMS sensors |
US7103477B1 (en) * | 2005-08-08 | 2006-09-05 | Northrop Grumman Corporation | Self-calibration for an inertial instrument based on real time bias estimator |
-
2007
- 2007-03-28 US US11/729,007 patent/US7640786B2/en active Active
-
2008
- 2008-03-07 EP EP08102372.3A patent/EP1975631B1/en not_active Not-in-force
- 2008-03-28 JP JP2008086549A patent/JP5275661B2/ja not_active Expired - Fee Related
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2013
- 2013-05-16 JP JP2013103643A patent/JP5639685B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP1975631A3 (en) | 2012-02-08 |
JP2013152253A (ja) | 2013-08-08 |
JP5275661B2 (ja) | 2013-08-28 |
US7640786B2 (en) | 2010-01-05 |
EP1975631B1 (en) | 2013-05-08 |
EP1975631A2 (en) | 2008-10-01 |
US20080236242A1 (en) | 2008-10-02 |
JP2008241715A (ja) | 2008-10-09 |
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