WO2005088317A1 - Sensoranordnung - Google Patents
Sensoranordnung Download PDFInfo
- Publication number
- WO2005088317A1 WO2005088317A1 PCT/EP2005/051213 EP2005051213W WO2005088317A1 WO 2005088317 A1 WO2005088317 A1 WO 2005088317A1 EP 2005051213 W EP2005051213 W EP 2005051213W WO 2005088317 A1 WO2005088317 A1 WO 2005088317A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- sensor
- sensor arrangement
- substrate
- sensors
- arrangement according
- Prior art date
Links
Classifications
-
- 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
- G01P15/0888—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 for indicating angular acceleration
-
- 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
- G01P15/18—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration in two or more dimensions
Definitions
- the invention relates to a sensor arrangement for detecting movements, which is designed as a monolithic arrangement.
- ESP driving stability regulations
- the variables that can be changed by the driver include the steering angle, the accelerator pedal position, the brake pressure, the lateral acceleration of the vehicle and the rotational speed of the individual vehicle wheels.
- a target yaw rate is calculated from the measured variables.
- a yaw rate sensor measures the actual value of the yaw rate, which is set in response to the driving maneuver.
- occupant protection devices serve to increase the safety of occupants in a motor vehicle. In the event of a significant number of accidents, only one motor vehicle is involved. In this type of accident, fatal injuries usually occur when the motor vehicle is concerned with its
- DE 199 62 687 C2 discloses a method and a system for determining the angular acceleration of a motor vehicle rotating about its longitudinal axis.
- the known method calculates the angular acceleration from the difference between the detected accelerations and the component of a distance vector perpendicular to the axis of rotation.
- DE 199 22 154 C2 discloses a device for generating electrical signals which represent the yaw rate, the acceleration and the roll rate of the vehicle body.
- Essential components of these known methods and devices are sensor arrangements that detect linear speeds and accelerations as well as rotation rates and rotational accelerations around different axes of an initial system that is fixed to the vehicle. In order to limit manufacturing costs, such sensor arrangements are manufactured as silicon micromechanical systems.
- the monolithic design of acceleration sensors for two or three spatial directions is known in the prior art. Such sensors are commercially available, for example, from the manufacturers VTI and Kionix.
- US Pat. No. 5,313,835 describes a monolithic arrangement which consists of a two-axis gyroscope, a one-axis gyroscope, a three-axis linear acceleration sensor and a microprocessor electronics.
- the biaxial gyroscope and the uniaxial gyroscope complement each other to form a gyroscope measuring in three spatial directions.
- the known sensor arrangement is suitable for measuring rotation rates and linear accelerations in three spatial directions.
- the sensor arrangement according to the invention for detecting movements is designed as a monolithic arrangement in which several sensors are integrated.
- a first sensor is provided for detecting a linear acceleration and a second sensor for detecting a rotation rate.
- the sensor arrangement is characterized in that it comprises a third sensor for detecting a rotational acceleration.
- the sensor arrangement can advantageously be formed on a single-crystalline substrate.
- the single-crystalline substrate consists of silicon. The advantage here is that silicon technology is mature, so that high-quality sensors can be produced at low costs.
- the sensors are designed as micromechanical structures in the substrate.
- the sensors on the substrate are aligned such that they are suitable for a corresponding installation position in a motor vehicle, the linear acceleration in the longitudinal direction of the motor vehicle, the yaw rate and the roll acceleration to measure the longitudinal axis of the motor vehicle.
- the yaw rate is an important input variable for driving dynamics controls, while the roll acceleration often controls the triggering of occupant protection systems that were described at the beginning.
- the sensor arrangement has a fourth sensor which is suitable for detecting a linear acceleration and is aligned on the substrate in such a way that it is also able to measure a linear acceleration transverse to the longitudinal axis of the vehicle.
- Lateral acceleration is another useful input variable for vehicle dynamics controls.
- the measuring direction of the sensors can be in the main plane spanned by the substrate, while in another embodiment the measuring direction of the sensors can be perpendicular to the main plane spanned by the substrate.
- the assembly comprises two sensor arrangements in which the measurement directions of the sensors lie in the main plane spanned by the substrate and the measurement directions of the the two sensor arrangements are oriented perpendicular to one another, and if the assembly comprises a further sensor arrangement in which the measuring direction of the sensors lie perpendicular to the main plane spanned by the substrate.
- FIGS. 1 a and 1 b illustrate the parameter symbols used and the reference directions
- 3a to 3c a schematic representation of the integration of the sensor arrangement in a package.
- FIG. 1 Each sensor is combined in the form of an arrow tion is shown with a parameter identifier.
- the arrow shows the measuring direction of the respective sensor.
- the arrow abstracts the presence of an associated measuring transducer, which is implemented, for example, using an etching technology in silicon.
- Such etching technologies for different systems are known in the prior art.
- a linear acceleration sensor LA (“linear accelerometer”) is symbolized.
- a positive sign means acceleration in the direction of the arrow.
- An angular rate sensor AR (English: “angular rate sensor”) is surrounded by a circle Arrow symbolizes, whereby the direction of rotation around the arrow direction is clockwise.
- a rotational acceleration sensor AA (English: “angular accelerometer”) is made with two circles around an arrow symbolizes, whereby the rotation takes place clockwise around the direction of the arrow.
- FIGS. 2a to 2d The building blocks of the sensor arrangement relate to embodiments based on micro-mechanical systems that are manufactured on the basis of silicon. Such techniques are known to the person skilled in the art and can be adapted accordingly for the present application of the invention.
- FIG. 2a shows a silicon chip 4 with an integrated structure of rotation rate sensor 5, linear acceleration sensor 6, rotational acceleration sensor 7 and linear acceleration sensor 8. Areas 5a, 6a, 7a, 8a symbolize associated transducer chip areas. A surface 4a symbolizes a coin-integrated electronic circuit for the operation or pre-stage operation of the measuring transducers 5, 6, 7.
- this module is used as an inertial measuring cell in a housing for an ESP application combined with a rollover protection (English: “rollover -protection ").
- the chip level is aligned parallel to the vehicle level or the surface of the earth.
- the measurement direction of the sensors 7, 8 coincides with the direction of travel of a vehicle in which the sensor arrangement is installed the vehicle the yaw rate, the roll acceleration, the longitudinal acceleration and the lateral acceleration
- This exemplary embodiment represents an advantageous combination of known sensors with a rotational acceleration sensor 7.
- FIG. 2b schematically shows a frequently required reduced embodiment of the internal measuring cell from FIG. 2a.
- the measuring cell comprises a chip 9, a rotation rate sensor 10, a linear acceleration sensor 11 and a rotation acceleration sensor 12.
- the measuring directions of the sensors 10, 11, 12 are oriented in the same way as the measuring directions of the corresponding sensors 5, 7, 8 of the inertial measuring cell described in FIG. 2a.
- 2c shows a module with a chip 13, a linear acceleration sensor 14, a rotational acceleration sensor 15 and a rotation rate sensor 16.
- the measuring directions of all three sensors 14, 15, 16 are realized “out of plane” according to the definition described above.
- FIG. 2d shows a module with a chip 17, which comprises a linear acceleration sensor 18, a rotation rate sensor 19 and a rotation acceleration sensor 20.
- the measuring directions of all three sensors are implemented "in plane" in accordance with the definition described above. '
- a chip 13 and two chips 17 are combined with one another in such a way that an inertial measuring cell is created which measures the rotation rate, the linear acceleration and additionally the rotation acceleration in all three spatial directions.
- the three chips are aligned “in plane” with respect to one another.
- the two chips 17 are rotated at a right angle to one another in the plane, so that their sensor measurement directions are oriented perpendicular to one another and orthogonal to the measurement directions of the sensors on the chip 13 are.
- FIG. 3 shows schematically in several exemplary embodiments the integration of several monolithic sensor arrangements according to the invention in a single packaging housing.
- a housing 21 encloses a sensor module 24, of the type described in connection with FIG. 2a or FIG. 2b, and an associated separate electronic circuit 25, which evaluates the sensor output signals.
- a housing 22 encloses a sensor module 26, of the type described in connection with Fig. 2a or 2b, and a separate electronic circuit 28 which evaluates the sensors of the module 26.
- the sensor module 26 contains a cointegrated electronic circuit 27.
- a housing 23 accommodates two sensor modules 29 a, 29 b according to FIG. 2 d, a module 30 according to FIG. 2 c and an associated electronic circuit 31.
- Devices 29a, 29b, 30 can contain additional coin-integrated electronic circuits.
- This arrangement is a concrete exemplary embodiment of an internal social measuring cell which measures the rotation rate, the linear acceleration and the rotation acceleration in all three spatial directions.
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Gyroscopes (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP05729516A EP1725880A1 (de) | 2004-03-16 | 2005-03-16 | Sensoranordnung |
US10/592,620 US20080039992A1 (en) | 2004-03-16 | 2005-03-16 | Sensor Arrangement |
DE112005000524T DE112005000524A5 (de) | 2004-03-16 | 2005-03-16 | Sensoranordnung |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004012688 | 2004-03-16 | ||
DE102004012688.7 | 2004-03-16 | ||
DE102004012686 | 2004-03-16 | ||
DE102004012686.0 | 2004-03-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2005088317A1 true WO2005088317A1 (de) | 2005-09-22 |
Family
ID=34963363
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2005/051213 WO2005088317A1 (de) | 2004-03-16 | 2005-03-16 | Sensoranordnung |
Country Status (3)
Country | Link |
---|---|
US (1) | US20080039992A1 (de) |
EP (1) | EP1725880A1 (de) |
WO (1) | WO2005088317A1 (de) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009010189A1 (de) * | 2009-02-23 | 2010-08-26 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Messgerät zur Bestimmung des Überlebensraumes in einem Kraftfahrzeug |
DE102011085727A1 (de) * | 2011-11-03 | 2013-05-08 | Continental Teves Ag & Co. Ohg | Mikromechanisches Element, Bauelement mit einem mikromechanischen Element und Verfahren zum Herstellen eines Bauelements |
CN110674567A (zh) * | 2019-08-23 | 2020-01-10 | 中国人民解放军63729部队 | 一种基于外测加速度的箭上动力情况判决方法 |
DE102008043475B4 (de) * | 2008-11-04 | 2020-06-18 | Robert Bosch Gmbh | Verfahren zum Steuern einer Einrichtung und Vorrichtung zum Steuern der Einrichtung |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2966587B1 (fr) * | 2010-10-22 | 2012-12-21 | Sagem Defense Securite | Dispositif inertiel comportant des capteurs inertiels de precisions differentes |
JP2018056228A (ja) * | 2016-09-27 | 2018-04-05 | ルネサスエレクトロニクス株式会社 | 半導体装置、システムインパッケージ、及び車載用システムインパッケージ |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5313835A (en) * | 1991-12-19 | 1994-05-24 | Motorola, Inc. | Integrated monolithic gyroscopes/accelerometers with logic circuits |
WO1994012886A1 (en) * | 1992-12-03 | 1994-06-09 | Saab Scania Combitech Ab | A device for measuring force components in monocristalline material, a method for manufacturing such a device and a use of such a device |
US5610337A (en) * | 1992-04-30 | 1997-03-11 | Texas Instruments Incorporated | Method of measuring the amplitude and frequency of an acceleration |
US20030216884A1 (en) * | 2001-12-17 | 2003-11-20 | Donato Cardarelli | Planar inertial measurement units based on gyros and accelerometers with a common structure |
-
2005
- 2005-03-16 EP EP05729516A patent/EP1725880A1/de not_active Withdrawn
- 2005-03-16 US US10/592,620 patent/US20080039992A1/en not_active Abandoned
- 2005-03-16 WO PCT/EP2005/051213 patent/WO2005088317A1/de not_active Application Discontinuation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5313835A (en) * | 1991-12-19 | 1994-05-24 | Motorola, Inc. | Integrated monolithic gyroscopes/accelerometers with logic circuits |
US5610337A (en) * | 1992-04-30 | 1997-03-11 | Texas Instruments Incorporated | Method of measuring the amplitude and frequency of an acceleration |
WO1994012886A1 (en) * | 1992-12-03 | 1994-06-09 | Saab Scania Combitech Ab | A device for measuring force components in monocristalline material, a method for manufacturing such a device and a use of such a device |
US20030216884A1 (en) * | 2001-12-17 | 2003-11-20 | Donato Cardarelli | Planar inertial measurement units based on gyros and accelerometers with a common structure |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008043475B4 (de) * | 2008-11-04 | 2020-06-18 | Robert Bosch Gmbh | Verfahren zum Steuern einer Einrichtung und Vorrichtung zum Steuern der Einrichtung |
DE102009010189A1 (de) * | 2009-02-23 | 2010-08-26 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Messgerät zur Bestimmung des Überlebensraumes in einem Kraftfahrzeug |
DE102011085727A1 (de) * | 2011-11-03 | 2013-05-08 | Continental Teves Ag & Co. Ohg | Mikromechanisches Element, Bauelement mit einem mikromechanischen Element und Verfahren zum Herstellen eines Bauelements |
CN110674567A (zh) * | 2019-08-23 | 2020-01-10 | 中国人民解放军63729部队 | 一种基于外测加速度的箭上动力情况判决方法 |
Also Published As
Publication number | Publication date |
---|---|
EP1725880A1 (de) | 2006-11-29 |
US20080039992A1 (en) | 2008-02-14 |
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