WO2007074168A1 - System for acquiring seismic data with six components - Google Patents
System for acquiring seismic data with six components Download PDFInfo
- Publication number
- WO2007074168A1 WO2007074168A1 PCT/EP2006/070254 EP2006070254W WO2007074168A1 WO 2007074168 A1 WO2007074168 A1 WO 2007074168A1 EP 2006070254 W EP2006070254 W EP 2006070254W WO 2007074168 A1 WO2007074168 A1 WO 2007074168A1
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- sensors
- motion sensors
- module
- motion
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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
- 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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
- G01V1/00—Seismology; Seismic or acoustic prospecting or detecting
- G01V1/003—Seismic data acquisition in general, e.g. survey design
Definitions
- the invention relates to a seismic data acquisition system capable of measuring translational and rotational movements.
- the invention relates more precisely to a seismic data acquisition system able to perform measurements of translation movements along three components independent of space, and rotation around these three components.
- the invention thus relates more precisely to a seismic data acquisition system capable of performing measurements according to six components of space, namely three of translation and three of rotation.
- Such a system is therefore called a six-component system or a complete wave system.
- the invention also relates to a method for performing this type of measurements.
- seismic data acquisition systems use seismic sensors, planted in the ground, such as a geophone or as an accelerometer, which are mass-spring type inertial sensors. These systems make it possible to measure the vertical component of a wave reflected by the different layers of the subsoil following a shaking of the terrain caused by a suitable means.
- surface waves are of the "Rayleigh wave” type, one of the characteristics of which is in particular the tilting (rotational movement) of the medium in which they propagate.
- An object of the invention is therefore to propose a system that allows both measurements of translation movements according to three components of space, preferably orthogonal, and of rotation around these same three components of space
- gyroscopes In order to know the rotational movements, various measuring systems are known, such as, for example, gyroscopes. These gyroscopes are either inertial, using a wheel rotating at high speed, or optical, as in the case of a Sagnac interferometer. These components are however relatively expensive and / or bulky.
- the present invention provides a seismic data acquisition system and method, the system being characterized in that it comprises means arranged so that they make it possible to measure translational movements of a medium according to three independent components of space and rotational movements around each of these three independent components, thus forming a six-component system.
- the seismic data acquisition system may furthermore have at least one of the following characteristics: the means forming a six-component system comprise at least six motion sensors; the motion sensors are translational movement sensors; the system comprises a module housing the motion sensors, which are arranged in almost any position and direction, so that a matrix A, connecting a vector m representing the movements measured by the sensors and a vector v representing the real movements of the medium, is invertible; the motion sensors are arranged in pairs so that the motion sensors of a pair of sensors are arranged relative to each other symmetrically with respect to the geometric center of the module; the motion sensors are arranged so that the geometric axis passing through the motion sensors of a pair of sensors is orthogonal to the geometric axis passing through the motion sensors of another pair of sensors; each motion sensor comprises a sensitive axis, the motion sensors of a pair of sensors being arranged so that their sensitive axes are parallel; the motion sensors are arranged so that the parallel sensitive axes of a pair of sensors are orthogonal with the parallel sensitive sensitive
- FIG. 2a shows schematically and in sectional view, a preferred embodiment, given by way of non-standard example limiting, a data acquisition system according to the invention, said system being subjected to a translational movement;
- Figure 2b shows the data acquisition system of FIG. 2a, according to the same sectional view, subjected to a rotational movement about an axis orthogonal to the direction of the translational movement of FIG. 2a;
- FIG. 3 is a schematic and perspective view of a preferred embodiment, given by way of non-limiting example, of a data acquisition system according to the present invention.
- FIG. 4 schematically and perspectively shows a data acquisition system according to an alternative and generalized embodiment of the invention.
- FIG. 1 shows a sectional view of a data acquisition system according to the prior art and formed of a module 1 comprising at its center a motion sensor 2 with a sensitive axis 3 and making it possible to carry out measurements of movements according to a single component of space. More precisely, this motion sensor 2 is able to measure a movement according to the vertical component (z axis) of the wave reflected in the different sub-layers following a shaking of the terrain caused on the surface.
- This motion sensor 2 is typically a geophone measuring the speed or an accelerometer.
- FIG. 2a and 2b show in sectional view a pair of motion sensors of a six-component seismic data acquisition system according to a preferred embodiment of the invention. The description made in support of these figures makes it possible to represent only part of the six-component system according to the invention, the system being only partially represented by the sectional view.
- This pair of motion sensors makes it possible to measure translational movements according to a first component of the space and rotational movements around another component of the space, orthogonal to the first component.
- the complete system will be described later, in support of Figure 3.
- the seismic data acquisition system represents a module 10 and two motion sensors
- the motion sensors 20, 30 are in accordance with a motion sensor used according to the state of the art and each comprise at least one sensitive axis, preferably only one, referenced respectively 41 and 42.
- the motion sensors 20, 30 are arranged relative to one another symmetrically with respect to the geometric center O of the module 10.
- the sensors 20, 30 are fixed on the module 10 of the data acquisition system so that their respective sensitive axes 41, 42 are parallel and preferably with a common direction and direction.
- the module is of parallelepipedal shape and preferably of cubic form. More precisely, the sensors 20, 30 are respectively fixed on two parallel and opposite faces 11, 12 of the module 10 of the data acquisition system, the sensitive axes 41 and 42 respectively belonging to the planes defined by these faces 11 and 12. More precisely, the sensors 20, 30 are fixed at the center of the faces 11, 12 of the module 10.
- the motion sensors 20, 30 may be speed or acceleration sensors. However, in the following description, and for the sake of simplification, only the case where the motion sensors 20, 30 are speed sensors is described.
- FIG. 2a the system according to the present invention partially shown with a pair of motion sensors 20, 30 is translated in the XZ plane of a medium 50.
- the two sensors 20 and 30 each make it possible to obtain a measurement of the speed linked to a translational movement, that is to say the speed of displacement of the medium in which the sensors are located, and more generally the data acquisition module 10.
- the first sensor 20 makes it possible to obtain a speed Vi and the second sensor 30 makes it possible for it to obtain a speed V 2 .
- the use of two sensors instead of a single sensor makes it possible to gain 3dB on the instrumental signal-to-noise ratio.
- this same system also partially represented with the pair of motion sensors 20, 30 is subjected to a rotational movement of the same medium 50 around the Y component orthogonal to the XZ plane passing through the center O of the module. 10
- the two sensors 20 and 30 each make it possible to obtain a measurement of the speed of rotation related to the rotational movement of the medium 50. Indeed, the sensors 20 and 30 undergo, under the effect of a rotational movement, a displacement in the opposite direction.
- the distance separating the centers Ci and C 2 of the motion sensors 20 and 30 is therefore 2R.
- the rotational movement which is acquired by the motion sensors 20, 30 of the data acquisition system can be achieved with a chosen precision. Indeed, the greater the distance separating the centers
- Ci and C 2 motion sensors 20 and 30 is important, the sensitivity to a rotational movement of the medium 50 is large. It is therefore quite possible to adapt the size of the data acquisition system according to the desired accuracy on the knowledge of the speed of rotation of the medium.
- FIG. 3 presents such a system schematically and for perspective view, according to a preferred embodiment.
- the six-component data acquisition system comprises means constituted by three pairs of motion sensors referenced 20, 30, and 21, 31 and 22, included in a module 10.
- Motion sensors are translational motion sensors.
- the motion sensors of a pair of sensors are arranged relative to one another symmetrically with respect to the geometric center O of the module 10.
- the module 10 employed is of parallelepipedal shape, and preferably of cubic form.
- each of the motion sensors 20, 30, 21, 31, 22, 32 is more preferably disposed in the center of the face 11, 12, 13, 14, 15, 16 respectively.
- the geometric axis Y1 passing through the motion sensors of a pair of sensors 20, 30 is orthogonal to the geometric axis X1 or Z1 passing through the motion sensors of another pair of sensors 21, 31 or 22, 32
- the respective sensitive axes of the motion sensors forming the pair in question are parallel and preferably oriented in the same direction and in the same direction.
- the parallel sensitive axes 41, 42 of a pair of sensors 20, 30 are orthogonal with the parallel sensitive axes 43, 44 on the one hand and 45, 46 on the other hand of another pair of sensors.
- the motion sensors 20 and 30 are respectively fixed on two parallel and opposite faces 11 and 12 of the module 10 and belonging to the plane XZ
- the motion sensors 21 and 31 are respectively fixed on two parallel and opposite faces 13 and 14 of the module 10 and belonging to the plane YZ
- the motion sensors 22 and 32 are respectively fixed on two parallel and opposite faces 15 and 16 of the module 10 and belonging to the plane XY, and this according to each of these pairs of motion sensors to the description made in support of Figures 2a and 2b.
- Each motion sensor 20, 30, 21, 31, 22, 32 is preferably a motion sensor with a single sensitive axis referenced respectively 41, 42, 43, 44, 45, 46.
- Calibration consists in obtaining the coefficients of matrix A.
- the motion sensors do not need to have a very precise sensitivity, since these sensitivity errors can be corrected. Thanks to this calibration, the geometric quality of the support as well as the positioning of the sensors on this support do not require extreme rigor since the defects are compensated by the method. The additional cost related to the calibration step is clearly offset by lower manufacturing constraints.
- an alternative embodiment as illustrated in FIG. 4, can provide a module and motion sensors arranged so that the sensors are arranged almost anywhere in the volume of the module 10, ie distances from the center O of the module 10 and with any orientation and direction.
- this module is calibrated according to the calibration method described above, it is possible to find the six motion components of the medium to which the module is subjected as precisely as with a parallelepipedal module as described above. if we apply the relation (El).
- the matrix A of calibration is invertible, which excludes a small number of singular positions of the sensors of movements, such as two sensors combined or all sensors in one or two planes.
- FIGS. 2a, 2b, 3 and 4 relate to means 20, 30, 21, 31, 22, 32 which are translational movement sensors, but it may be envisaged to use as motion sensors at least three translational motion sensors and at least three rotational motion sensors.
- the system according to the invention can also provide means for forming a six-component system, other means such as for example one or more sensors selected from, by way of non-limiting example, a pressure sensor and / or a temperature sensor.
- the present invention pertaining to the six-component seismic data acquisition system is not limited to the embodiments described above but extends to any embodiment within its spirit.
- any embodiment of a seismic data acquisition system that makes it possible to obtain six independent measurements corresponding to the three translation components along the three directions of space and to the three rotational movements around three other components of space, ie around the three directions of space.
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- General Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Environmental & Geological Engineering (AREA)
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Abstract
Description
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Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA2635385A CA2635385C (en) | 2005-12-29 | 2006-12-28 | System for acquiring seismic data with six components |
GB0812114A GB2447001B (en) | 2005-12-29 | 2006-12-28 | System for acquiring seismic data with six components |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0513444 | 2005-12-29 | ||
FR0513444A FR2895801B1 (en) | 2005-12-29 | 2005-12-29 | SYSTEM FOR ACQUIRING SEISMIC DATA WITH SIX COMPONENTS |
US11/349,333 | 2006-02-08 | ||
US11/349,333 US7474591B2 (en) | 2005-12-29 | 2006-02-08 | Six-component seismic data acquisition system |
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WO2007074168A1 true WO2007074168A1 (en) | 2007-07-05 |
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PCT/EP2006/070254 WO2007074168A1 (en) | 2005-12-29 | 2006-12-28 | System for acquiring seismic data with six components |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7474591B2 (en) * | 2005-12-29 | 2009-01-06 | Sercel | Six-component seismic data acquisition system |
CN101738633A (en) * | 2009-12-18 | 2010-06-16 | 陈�峰 | High-accuracy deep-well six-dimensional seismograph |
WO2010122400A3 (en) * | 2009-04-22 | 2011-01-06 | Schlumberger Technology B.V. | Methods and systems for borehole seismic measurements |
CN106767805A (en) * | 2017-01-08 | 2017-05-31 | 上海拓攻机器人有限公司 | High accuracy inertia measuring method and measuring system based on MEMS sensor array |
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FR2107847A1 (en) * | 1970-09-21 | 1972-05-12 | Consiglio Nazionale Ricerche | Device for detecting and measuring angular movements, applicable to inertial navigation |
FR2594957A1 (en) * | 1986-02-21 | 1987-08-28 | Schilling Franz | Accelerometer with six degrees of freedom using electromagnetical suspension |
US5383363A (en) * | 1993-02-10 | 1995-01-24 | Ford Motor Company | Inertial measurement unit providing linear and angular outputs using only fixed linear accelerometer sensors |
US20030079358A1 (en) * | 2000-07-06 | 2003-05-01 | Nai Kenneth Cheng-Hoe | Method of an apparatus for correction of coordinate measurement errors due to vibrations in coordinate measuring machines (cmms) |
WO2005121812A1 (en) * | 2004-06-09 | 2005-12-22 | ETH Zürich | Multi-axis capacitive transducer and manufacturing method for producing it |
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2006
- 2006-12-28 WO PCT/EP2006/070254 patent/WO2007074168A1/en active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
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FR2107847A1 (en) * | 1970-09-21 | 1972-05-12 | Consiglio Nazionale Ricerche | Device for detecting and measuring angular movements, applicable to inertial navigation |
FR2594957A1 (en) * | 1986-02-21 | 1987-08-28 | Schilling Franz | Accelerometer with six degrees of freedom using electromagnetical suspension |
US5383363A (en) * | 1993-02-10 | 1995-01-24 | Ford Motor Company | Inertial measurement unit providing linear and angular outputs using only fixed linear accelerometer sensors |
US20030079358A1 (en) * | 2000-07-06 | 2003-05-01 | Nai Kenneth Cheng-Hoe | Method of an apparatus for correction of coordinate measurement errors due to vibrations in coordinate measuring machines (cmms) |
WO2005121812A1 (en) * | 2004-06-09 | 2005-12-22 | ETH Zürich | Multi-axis capacitive transducer and manufacturing method for producing it |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7474591B2 (en) * | 2005-12-29 | 2009-01-06 | Sercel | Six-component seismic data acquisition system |
WO2010122400A3 (en) * | 2009-04-22 | 2011-01-06 | Schlumberger Technology B.V. | Methods and systems for borehole seismic measurements |
US8255164B2 (en) | 2009-04-22 | 2012-08-28 | Schlumberger Technology Corporation | Methods and systems for borehole seismic |
CN101738633A (en) * | 2009-12-18 | 2010-06-16 | 陈�峰 | High-accuracy deep-well six-dimensional seismograph |
CN106767805A (en) * | 2017-01-08 | 2017-05-31 | 上海拓攻机器人有限公司 | High accuracy inertia measuring method and measuring system based on MEMS sensor array |
CN106767805B (en) * | 2017-01-08 | 2023-08-18 | 上海拓攻机器人有限公司 | High-precision inertial measurement method and measurement system based on MEMS sensor array |
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