• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The invention proposes an accelerometer device for determining the acceleration of an object to which the accelerometer device is mechanically connected, along 3 X, Y and Z axes of a main orthonormal reference system (X, Y, Z) comprising three axes. X, Y, Z, said object being subjected to a surrounding pressure. The device comprises a number N of MEMS type accelerometer sensors (11, 12), said number N of accelerometer sensors being at least two, each sensor (11, 12) being defined by construction in an auxiliary reference system comprising 3 orthonormal axes (Xi, Yi, Zi), said set of accelerometer sensors comprising at least one pair of sensors mounted opposite head and substantially parallel to each other, and: - for each of the pair of accelerometer sensors, the sensors present two by two components of opposite sign along two axes of the main reference system; and the axes of the reference system according to which the components of the accelerometer sensors are two to two opposite on all the pairs of sensors comprise at least two of the three axes X, Y and Z of the reference system, which makes it possible to compensate the effect of the pressure on at least two axes of the reference system.
    公开号:FR3023920A1
    申请号:FR1401618
    申请日:2014-07-18
    公开日:2016-01-22
    发明作者:Christophe Robert；Thomas Fini；Fabienne Lebreil；Gras Herve Le；Isabelle Tournoud
    申请人:Thales SA；
    IPC主号:
    专利说明:

    [0001] FIELD OF THE INVENTION The invention generally relates to measuring systems, and in particular to an accelerometer device for measuring the 3-axis acceleration of an object mechanically connected to a measuring system. PRIOR ART Surface buildings or submarines are generally equipped with acoustic antennas for transmitting and / or receiving acoustic signals propagating in the sea. An acoustic antenna is formed of a set of sensors (hydrophones). separately accessible, that is to say whose outputs can be combined in different ways. The acoustic antennas thus comprise a set of hydrophones which can be arranged in the acoustic modules of the antenna according to different combinations depending on the configuration of the antenna. For example, a Towed Linear Acoustic Antenna (ALR or flute antenna) has a significant length that can measure a few hundred meters and has a small diameter. Such an antenna is towed by a towing cable several hundred meters and is intended to be submerged to deep enough depths in the sea (the pressure is of the order of 1 Bar every 10 meters of bottom). Because of its length, such an antenna includes a large number of hydrophones regularly distributed along the antenna in acoustic modules. It is known, for example, to arrange an elementary acoustic multi-sensor along the flute antenna in a separate acoustic module in order to remove the right / left ambiguity in underwater acoustics. Each acoustic module is protected by a small protective module due to the small diameter of the flute antenna. Each independent multi acoustic sensor is mounted on a printed circuit board (concentrator system) at one end thereof and perpendicular to the plane of the card. The acoustic module may furthermore comprise a plurality of auxiliary equipment such as direction and depth sensors, and electronic equipment that is mounted on the concentrator system, in the reduced space delimited by the protection enclosure of the acoustic module. The multi acoustic sensors in this case are designed to provide electrical signals proportional to the dynamic pressures exerted on them. However, their accelerometric sensitivity must be known for the signals supplied to be referenced according to the terrestrial acceleration forces. This acceleration reference is obtained by using an acceleration sensor (also called an accelerometer) mounted on the concentrator in association with each multi acoustic sensor and providing a signal representative of the acceleration of the flute along two axes and compensating for the effect of this acceleration differentially on the signals provided by each multi acoustic sensor. Such an accelerometer makes it possible to determine the biaxial acceleration of the object to which it is attached for a horizontal antenna.
    [0002] Such accelerometers have a significant cost. In particular, in the case of a flute antenna, the accelerometers are generally arranged in a known manner along the antenna, generally every 2 meters for interpolation. Moreover, for each multi acoustic sensor, an accelerometer is provided on the same concentrator with other electronic components of the acoustic module to avoid interpolation. Given the length of the antenna, the number of accelerometers required and consequently the cost induced by all these accelerometers can be very important. Another disadvantage of these accelerometers is their size relative to the volume of the enclosure of the acoustic module (itself limited by the small diameter of the flute antenna). In particular, it may be useful to stack several printed circuit boards and integrate them in each acoustic module by connecting the multi acoustic sensor on each of the stacked cards, which ensures the continuity of operation of the multi-sensor in case of failure. However, the current size of conventional accelerometers (in the direction perpendicular to the axis of the antenna) and their number would not allow such a stack.
    [0003] General definition of the invention The invention improves the situation. For this purpose, it proposes an accelerometer device for determining the acceleration of an object to which the accelerometer device is mechanically connected, along 3 X, Y and Z axes of a main orthonormal reference system (X, Y, Z) comprising three axes X, Y, Z, said object being subjected to a surrounding pressure. The device comprises a number N of MEMS type accelerometer sensors, the number N of accelerometer sensors being at least equal to two, each sensor being defined by construction in an auxiliary reference system comprising 3 orthonormal axes (Xi, Yi, Zi), the set of accelerometer sensors comprising at least one pair of sensors mounted opposite head and substantially parallel to each other, and: for each of the pairs of sensors, the sensors present two by two components of opposite sign along two axes of the reference system main ; and the axes of the reference system according to which the components of the accelerometer sensors are two to two opposite on all the pairs of sensors comprise at least two of the three axes X, Y and Z of the reference system, which makes it possible to compensate the effect of the pressure on at least two axes of the reference system. According to another characteristic, the device may comprise a processing unit for calculating the average of the accelerations along each axis X, Y and Z, the average of the accelerations along a given axis being determined from the accelerations determined by each accelerometer sensor according to the given axis. Calculation of the average of the accelerations along a given axis may also take into account the gain and / or the offset of each predetermined sensor in a unit calibration phase implemented separately for each sensor 30 before mounting. Calculating the average of the accelerations along a given axis may also take into account a predefined gain compensation factor.
    [0004] In one embodiment, the set of sensors may comprise two accelerometer sensors connected to at least one printed circuit board, while the axes of the reference system in which the sensor components are two to two opposite on all the sensors. The sensors comprise two of the X, Y and Z axes of the reference system, which makes it possible to correct the effect of the pressure exerted on the object along the two axes. In another embodiment, the set of accelerometer sensors may comprise three sensors, while the axes of the reference system in which the sensor components are two to two opposite on all of the sensors comprise the three axes X, Y and Z of the reference system, which makes it possible to correct the effect of the pressure exerted on the object along the three axes. According to one characteristic of the invention, the object may be an acoustic antenna comprising a set of multi acoustic sensors, each multi acoustic sensor being mounted on at least one printed circuit board while the accelerations determined by the accelerometer device according to each axis. X, Y and Z are used to compensate for the effect of acceleration of the acoustic antenna on the position of the multi acoustic sensor. Sensors may have different sensitivity to pressure.
    [0005] The invention also proposes an acoustic module for an acoustic antenna extending along a main axis, comprising an accelerometer device according to one of the preceding characteristics, the accelerations determined by the accelerometer device along each axis X, Y and Z being used to compensate for the effect of the acceleration of the acoustic antenna on the position of the multi acoustic sensor. The acoustic sensor may be a multi acoustic sensor axis substantially parallel to the axis of the antenna. The acoustic module may comprise at least one printed circuit board on which the accelerometer sensors are mounted.
    [0006] The module may comprise a plurality of printed circuit boards, stacked substantially perpendicular to the axis of the antenna, on which the accelerometer sensors are mounted. The invention further provides an acoustic antenna comprising a set of acoustic modules according to one of the preceding features. The invention thus provides an accelerometer device with a small footprint. The use of such a device in an acoustic module of an antenna thus makes it possible to stack several printed circuit boards in one and the same module.
    [0007] Another advantage of the accelerometer device according to the invention is its low cost. Such a device is thus particularly suitable for use in antennas using a large number of acoustic modules. The accelerometer device also makes it possible to maintain the system by its self-referencing, that is to say the comparison with respect to a double reference and a calibration with respect to the acceleration of gravity. DESCRIPTION OF THE FIGURES Other characteristics and advantages of the invention will become apparent with the aid of the description which follows and the figures of the appended drawings in which: FIG. 1 represents an example of an environment in which certain embodiments of the invention; FIG. 2 is a schematic representation of the acoustic modules of a flute antenna, according to certain embodiments of the invention; FIG. 3 is a schematic view of the accelerometer device according to one embodiment of the invention; FIG. 4 shows the head-to-side positioning of the accelerometer sensors in a main reference system, according to one embodiment of the invention; FIG. 5 represents an accelerometer device with 3 accelerometer sensors in a main reference system, according to another embodiment of the invention; FIG. 6 is a schematic representation of the acoustic modules of a flute antenna comprising accelerometer devices with 3 accelerometer sensors, according to one embodiment of the invention; FIG. 7 is a view from above of the head-opposed accelerometer sensors in the main reference system, according to an embodiment of the invention; FIG. 8 is a diagram illustrating the processing of the signals measured by the head-opposed accelerometer sensors, according to one embodiment of the invention; and FIG. 9 is a flowchart showing the reference calculation steps according to each axis of the main reference system, according to an embodiment of the invention. The drawings and appendices to the description may not only serve to better understand the description, but also contribute to the definition of the invention, if any.
    [0008] DETAILED DESCRIPTION FIG. 1 represents an example of an environment in which certain embodiments of the invention may be implemented.
    [0009] Surface buildings or submarines 2 are generally equipped with a set of acoustic antennas for transmitting and / or receiving acoustic signals in the seabed, for example flute antennas 10 which have a freedom of movement , distributed antennas or flanked antennas. To facilitate the description of the embodiments of the invention, the following description will be made with reference to a flute antenna 10 by way of non-limiting example.
    [0010] FIG. 2 represents a section of a flute antenna 10 comprising a set of acoustic modules 100. The flute antenna 10 furthermore comprises a set of acoustic sensors 101 (for example of the hydrophone type) regularly distributed along the antenna in acoustic modules 100. In the embodiment of FIG. 2, an acoustic sensor 101 is arranged at regular intervals along the flute antenna in a distinct acoustic module 100. In each acoustic module 100, comprising one or more acoustic sensors 101, is arranged at least one printed circuit board 102 (also called "concentrator system"), for example of generally rectangular shape, along the axis of the antenna. Acoustic sensors 101 may for example be multi acoustic sensors. In a particular embodiment, the sensors 101 of acoustic multi-sensor type 101 may comprise N hydrophones, situated in a plane perpendicular to the axis A of the linear antenna, and distributed over a circle centered on the axis of the antenna. antenna and having a diameter smaller than the diameter of the antenna. Each acoustic sensor 101 may be mechanically and electrically connected to at least one card 102 for its electrical interface. Alternatively, each acoustic module 100 may comprise a plurality of printed circuit boards stacked in the direction perpendicular to the axis of the antenna, and mechanically and electrically connected to the acoustic sensor 101 so that in case of failure of the one of the cards the other cards can continue to interface the acoustic sensor. The mechanical position of each card 102 is rigidly connected to the acoustic sensor 101. The remainder of the description will be made with reference to a single printed circuit board 102 and to an acoustic sensor 101 of multi-sensor type, as a non-limiting example. Each acoustic module 100 can be protected by a speaker 103 (also called "acoustic centraliser") of small dimensions. The height of the enclosure 103 may for example be limited by the small diameter of the antenna 10, in the case of a flute antenna. Each acoustic sensor 101 may be mounted on the concentrator system 102. In FIG. 2, each acoustic multi-sensor 101 is mounted at one end of the concentrator system and perpendicular to the plane of the concentrator to optimize the occupation of the space defined by the enclosure 103 of the acoustic module. The multi acoustic sensors are configured to provide electrical signals proportional to the dynamic pressures exerted on them. Each acoustic module 100 may furthermore comprise a plurality of auxiliary electronic equipment.
    [0011] The flute antenna 10 may in particular be provided with a protective envelope 104 intended to protect the electronic equipment. It may contain in particular a liquid of lighter density than water and very high resistivity (such as oil) to limit crushing of the envelope and its contents. Such a liquid makes it possible in particular to confer a substantially zero buoyancy to the antenna and to put the antenna in equipression with the outside. According to one aspect of the invention, each acoustic module 100 may comprise an accelerometer device 1 for determining the acceleration of the antenna 10 along 3 axes X, Y and Z defining a main orthonormal reference system and to compensate for the effect of the acceleration on the signal provided by each multi acoustic sensor 101. In the applications of the invention to acoustic antennas, the X axis corresponds to the roll axis, the Z axis corresponds to the pitch axis and the Y axis corresponds to the yaw axis.
    [0012] Figure 3 is a schematic view of the accelerometer device 1 according to one embodiment of the invention showing the main reference system (X, Y, Z). The accelerometer device 1 comprises a set of digital accelerometer sensors 11, 12 of the electron microsystem type (also called MEMS in relation to the English expression "microelectromechanical systems").
    [0013] The MEMS accelerometer sensors 11 and 12 may be mounted on at least one printed circuit board 102 and substantially parallel to each other. The accelerometer sensors may for example be of generally rectangular shape and of very low height. In one embodiment, the accelerometer device may be rigidly mounted on the same printed circuit boards 102 as the acoustic sensor 101. In the following description of some embodiments, reference will be made to a printed circuit board. 102 commonly connected to the acoustic sensor 101 and the accelerometer device 1 as an illustrative example.
    [0014] According to one aspect of the invention, the accelerometer device 102 comprises at least one pair of accelerometer sensors 11 and 12 arranged head-opposite to each other. The sensors 11 and 12 may have a different sensitivity to the pressure. In one embodiment, the pair of head-opposing sensors comprises two sensors 11 and 12 arranged on either side of the printed circuit board 102 (also referred to as "upper sensor" and "lower sensor" respectively) as shown in FIG. FIG. 3. Each accelerometer sensor 11 and 12 is associated by construction with a sensor reference system (Xi, Yi, Zi) which makes it possible to define the positioning of the accelerometer sensor. The plane (Xi, Yi) defines the plane of each accelerometer sensor. Each accelerometer sensor is arranged in the device 1 so that its plane (Xi, Yi) is parallel to the plane (X, Z) of the reference system.
    [0015] The accelerometer sensors 11 and 12 mounted in opposition may be opposite one another with respect to the axis of the antenna or arranged at a distance d chosen relative to each other with respect to the axis of the antenna. the antenna, as shown in Figure 4. The distance d can be chosen according to the orientation of the support plane (for example, it may be more or less important depending on whether or not the support plane is parallel). Moreover, the fixing of the accelerometers on the card 102 (for example welding type fixing) can be carried out so as to contain the errors. In the examples shown in Figures 3 and 4, the reference system of the upper sensor 11 is noted (X1, Y1, Z1) while the reference system of the lower sensor 12 is noted (X2, Y2, Z2). The relative head-opposite positioning of the two sensors 11 and 12 is such that the respective axes Z1 and Z2 of the first sensor 11 and the second sensor 12 are parallel and of opposite signs. As used herein in connection with an N-sensor accelerometer device, the term "opposite-head" refers to the mounting of the accelerometer sensors among the N sensors such that: - for each pair of sensors considered, the sensors have two by two of the components of opposite sign along two axes of the main reference system (for example, the axis Z1 of the upper accelerometer sensor 11 corresponds to the axis -Z2 of the lower accelerometer sensor 12 and the axis Y1 of the accelerometer sensor upper 11 corresponds to the axis -Y2 of the lower accelerometer sensor 12), and the axes of the main reference system in which the components are opposite for the set of sensor pairs comprise at least two of the three axes X, Y and Z of the reference system. Such a positioning of the sensors makes it possible to correct the effect of the pressure exerted on the antenna on at least two axes. With reference to FIG. 4, the positioning of the accelerometer sensors 11 and 12 with respect to the main reference system (X, Y, Z) is such that: the axis X1 of the first accelerometer sensor 11 coincides with the axis -Z the main reference system; The axis Y1 of the first accelerometer sensor 11 coincides with the axis X of the main reference system; the axis Z1 of the first accelerometer sensor 11 coincides with the axis -Y of the main reference system; the axis X2 of the second accelerometer sensor 12 coincides with the axis -Z of the main reference system; the axis Y2 of the second accelerometer sensor 12 coincides with the axis -X of the main reference system; the axis Z2 of the second accelerometer sensor 12 coincides with the Y axis of the main reference system. Thus, when the accelerometer device comprises two sensors 11 and 12 (2D assembly), the head-to-side assembly of the two accelerometer sensors is such that the two sensors have components of opposite sign along two axes of the main reference system (for example the axis + Z1 of the upper accelerometer sensor 302 3 920 11 11 corresponds to the axis -Z2 of the lower accelerometer sensor 12 and the axis + y1 of the upper accelerometer sensor 11 corresponds to the axis -Y2 of the lower accelerometer sensor 12 ). Thus, 2 axes on the 3 axes of the main reference system are opposite (Y corresponding to the direction of the axes Z1 / Z2 and X corresponding to the direction of the axes Y1 / Y2), which makes it possible to compensate the effect of the pressure along these 2 axes. Figure 5 shows an accelerometer device with 3 sensors. The positioning of the accelerometer sensors 11, 12 and 13 with respect to the main reference system (X, Y, Z) is such that: the axis X 1 of the first accelerometer sensor 11 coincides with the axis -Z of the main reference system ; the axis Y1 of the first accelerometer sensor 11 coincides with the axis X of the main reference system; The axis Z1 of the first accelerometer sensor 11 coincides with the axis Y of the main reference system; the axis X2 of the second accelerometer sensor 12 coincides with the axis -Z of the main reference system; the axis Y2 of the second accelerometer sensor 12 coincides with the axis -X of the main reference system; the axis Z2 of the second accelerometer sensor 12 coincides with the Y axis of the main reference system; the axis X3 of the third accelerometer sensor 13 coincides with the Z axis of the main reference system; The axis Y3 of the third accelerometer sensor 13 coincides with the axis -X of the main reference system; the axis Z3 of the third accelerometer sensor 13 coincides with the axis -Y of the main reference system. The components of each sensor pair thus have opposite sign components. Thus, for the pair {11, 12}, the axes Y1, Y2 of the first and second sensors 11 and 12 are opposite (corresponding to the direction of the X axis of the reference system); and the axes Z1, Z2 of the first and second sensors 11 and 12 are opposed (corresponding to the direction of the Y axis of the reference system). For the pair {11, 13}, the axes X1, X3 of the first and third sensors 11 and 13 are opposite (corresponding to the direction of the Z axis of the reference system); and the axes Y1, Y3 of the first and third sensors 11 and 13 are opposed (corresponding to the direction of the Y axis of the reference system).
    [0016] For the pair {12, 13}, the axes X2, X3 of the second and third sensors 12 and 13 are opposed (corresponding to the direction of the Z axis of the reference system); and the axes Z2, Z3 of the second and third sensors 12 and 13 are opposed (corresponding to the direction of the Y axis of the reference system).
    [0017] As a variant, the third sensor 13 may be mounted in opposition along the axis Y with respect to the first sensor 11: the axes Z2 and Z3 of the second accelerometer sensor 12 and the third accelerometer sensor 13 respectively are then parallel and of opposite sign to the Z1 axis of the first accelerometer sensor 11, which corresponds to two pairs of accelerometer sensors mounted head-opposite: 11/12 and 11/13. Similarly, the sensor 13 can be positioned at the sensor 12. Thus, when the accelerometer device comprises 3 sensors 11, 12 and 13 (3D), as illustrated in the examples of FIGS. 5 and 6, the opposite head assembly of the three accelerometer sensors are such that: - for each pair of sensors considered, for example {12, 13} and {11, 12}, the sensors have two-by-two components of opposite sign along two axes of the main reference system (for example: example Z3 / Z2 and X3 / X2 for the pair {12, 13} or Z1 / Z2 and Y1 / Y2 for the pair {11, 12}), and -the axes of the main reference system in which the components are opposite on the set of sensor pairs comprise the three X, Y and Z axes of the reference system.
    [0018] Thus, the components along the three axes X, Y, Z are opposite on all the pairs, which makes it possible to compensate the effect of the pressure on the 3 axes. It should be noted that although a number of sensors equal to three is sufficient to compensate for the effect of the pressure on the three axes, the device may include a greater number of accelerometer sensors. FIG. 7 shows a schematic view from above of the three accelerometer sensors 11, 12 and 13 of FIG. 5. In the example represented, each accelerometer sensor is a sensor of the ADXL346 type, LGA format (acronym for the English expression " Land Grid Array ") and comprises 16 connection pins denoted 1 to 16. The use of such a device makes it possible not only to compensate the effect of the acceleration on the signals supplied by the multi acoustic sensors but also to make the MEMS type accelerometer sensors 11, 12, 13 insensitive to the pressure P which is exerted on them. Indeed, the MEMS are very sensitive to the pressure so that at large immersion depths they can provide an estimate of the very biased acceleration due to the strong pressure exerted. The equi-pressure in the sheath is applied to the incompressible oil and to the MEMS (for example, it has been observed that at 100Bar a substantially 20% error is obtained on an isolated MEMS). By mounting the MEMS type accelerometer sensors in a head-opposite configuration, for each pair such as, for example, the pair {11, 12}, the reference difference due to the pressure exerted on the first sensor 11 (top sensor) is opposite sign to the referencing gap due to the pressure exerted on the second sensor 12.
    [0019] This makes it possible to compensate the effect of the pressure exerted on the acoustic module on at least two axes. FIG. 8 represents a schematic view of the antenna section 10 comprising three acoustic modules M1, M2, M3 (100) showing the processing architecture of the signals measured by the sensors, according to an exemplary embodiment of the invention. In the example shown, only the module M2 is equipped with an accelerometer device 1 with two sensors providing three-axis accelerations S1 and S2 and an associated acoustic sensor 101 (the elements 1 and 101 are not represented on the Figure 6). The accelerometer device 1 may comprise a processing unit 15 (for example of the FPGA type) configured to calculate an average (also referred to as a "reference") on each of the X axes. , Y and Z of the accelerations measured by each pair of head-opposed accelerometer sensors (11, 12) of the device 1 (average of the components of opposite signs). For example in embodiments where the device comprises more than N accelerometer sensors, including a head-opposed pair, mounted such as N-1 accelerometer sensors (upper sensors) are arranged on the upper part of the board while 1 sensor is mounted on the lower part (lower sensor), (N-1) pairs can be considered for the calculation of references per axis, each pair comprising one of the (N-1) upper sensors and the lower sensor. The references thus calculated make it possible to reduce the acceleration difference due to the static pressure P which is exerted along each axis on the acoustic antenna. In some embodiments, the processing unit 15 may be used to calibrate the values of the accelerations along the 3 X, Y and Z axes prior to mounting the MEMS accelerometer sensors 11 and 12 and to improve the accuracy of the final estimate. 3-axis acceleration. The calibration makes it possible in particular to determine the positioning error with respect to the coding of each MEMS accelerometer sensor 11 and 12 (mechanical calibration). Moreover, on the electrical front, the accelerometer sensors may not be identical and locally in a stable position so that the measurements can be altered. The electrical calibration of the accelerometer sensors makes it possible to compensate the architecture for the expected values in terms of gain and offset. For example, by choosing as a reference the support of the acoustic sensor the value expected for 1g is 256 and -1g -256 for each coordinate of the reference.
    [0020] In the example of FIG. 8, the processing unit 15 of the accelerometer device of the module M2 (FPGA) makes it possible to calibrate the accelerometer sensors 11, 12 by averaging the respective accelerations measured along the three axes S1 = (X1, Y1, Z1) and S2 = (X2, Y2, Z2) from previously calculated calibration parameters. In one embodiment, each accelerometer sensor may be individually calibrated (separately).
    [0021] The calibration method may comprise the following steps: before the mounting of the accelerometer device 1, for each accelerometer sensor 11 and 12 of the device 1, the calibration parameters (gains and offset) are estimated for each axis X, Y, Z to from a series of measurements. In particular, an acceleration of 1 * g along each accelerometer sensor axis is encoded into a known output value at the sensor output in the relevant direction (the expected output value may be for example "256 "). The measurements made along each axis for each accelerometer sensor 11, 12 of the device and the comparison of the measurements with the expected value (eg "256") then make it possible to estimate the offset ("offset" in the English language) and the gain of each sensor along each axis. The gain and the estimated offset for each sensor and for each accelerometer sensor axis 11, 12 of the device 1 (also called "calibration parameters") can then be stored in memory among the constants of the FPGA device 15. -in real conditions for example at sea, the FPGA processing device 15 can process the input acceleration values which comprise 3 values per accelerometer sensor 11, 12 of the accelerometer device 1, these 3 values corresponding to an acceleration value by X axis , Y or Z. Thus for an accelerometer device 1 provided with 2 MEMS accelerometer sensors, 6 values will be processed. This method of processing consists in calibrating all of these acceleration values (at least 6 values) using the predetermined calibration parameters during the calibration phase at the time of manufacture of the device 1 (stored in the FPGA device 15). . More precisely, for each axis X, Y and Z, the average of the pairs of calibrated values is calculated for each pair of accelerometer sensors 11 and 12 comprising two head-opposed sensors.
    [0022] The preliminary calibration phase increases the accuracy and reduces the error offset. It also makes it possible to test the embedded function, in particular during integration and in the maintenance phase for different types of MEMS accelerometer sensors, which makes it possible to reduce the risks.
    [0023] It should be noted that the initial calibration phase is an optional phase that may or may not be implemented depending on the desired accuracy. In addition, the acoustic antenna may include an adapter module 16 for applying a gain compensation factor G (also called scale factor) which may be applied to rescaling the calibrated acceleration values (averages calculated for each axis). The scale factor G makes it possible to adapt the dynamics of the numbers to be able to perform the calculations with a simpler calculator (for example with integers and not numbers with commas).
    [0024] Fig. 9 is a flowchart showing the method for calculating the calibrated acceleration values for an accelerometer device 1 to 3 accelerometer sensors comprising at least two head-to-side sensors (k pairs of accelerometer sensors). The method can be implemented at a chosen period (for example every 50 ms). The method is in particular implemented for each pair of MEMS accelerometer sensors (arranged in a head-opposite arrangement) of the accelerometer device 1. To facilitate the understanding of the description which follows, the following notations are defined for each of the k pairs of accelerometer sensors of the accelerometer device 1 (a pair consists of two sensors arranged opposite-head comprising an upper sensor, eg 11, and a lower sensor, eg 12): bx, k, sup, by, k, sup, bz, k, sup respectively denote the shifts of the upper head-opposite accelerometer sensor (eg 11) along each axis X, Y, Z; - bx, k, inf, by, k, inf, bz, k, inf respectively denote the reference shifts of the lower head-opposite accelerometer sensor (e.g. 12) along each axis X, Y, Z; 5 - gx, k, sup, gy, k, sup, gz, k, sup respectively denote the gains of the upper head-opposite accelerometer sensor (e.g., 11) along each X, Y, Z axis; - gx, k, inf, gy, k, inf, gz, k, inf respectively denote the gains of the upper head-opposite accelerometer sensor (e.g., 12) along each axis X, Y, Z; and - G denotes the scale factor to compensate the gain. In step 900, each accelerometer sensor of the accelerometer device 1 is calibrated before mounting the sensors to determine the gain and offset of each accelerometer sensor along each axis of the sensor Xi, Yi, Zi (calibration parameters). In step 901, the calibration parameters are then stored in the processing unit 15. When the device 1 is mounted on an acoustic antenna, in step 902, the accelerations can be measured by each sensor according to each axis. X, Y and Z. In step 903, for each pair k comprising two head-to-side sensors (for example 11, 12 and 12, 13 in the example of FIG. 5), the acceleration components Xk, Yk and Zk calibrated along each axis X, Y or Z are determined by averaging the values measured by the different sensors along the corresponding axis. The calculation of the average on each axis can take into account the calibration parameters such as the gain and / or the offset of each sensor along the axis and / or the factor G. In one embodiment, the components of acceleration Xk, Yk can be obtained according to the following equations: (171c, 1 by, k, 1) * 1 (17k, 2 by, k, 2) * 1 X gy, k, 1 gy, k, 2k = G * 2 and Zk means - (Zk -bz, k, i) * 1 ± (Zk, 2 gz, k, 1 Yk = G * bz, k, 2) * 1 gz, k, 2 2 k 1 bxk 1) 1 1 * k 2 bxk 2 i * Zk = G * gx, k, 1 gx, k, 2 Those skilled in the art will understand that steps 900 and 901 are performed prior to steps 902 and 903 without limitation of time. Moreover, the skilled person will understand that the values obtained in step 901 can be used for several measurements according to steps 902 and 903. The accelerometer device 1 based on MEMS sensors according to the embodiments of the invention allows thus to compensate for the effect of the pressure P exerted on the antenna. The inventors have in particular carried out pressure tests from 0 to 60 bars over 35 tests with MEMS accelerometer sensors of 8 different types. In the context of such tests, it has been observed on the X and Y axes a reference offset + -1 lsb (standard deviation of 0.3) and on the Z axis a referencing offset of + -2 Isb ( standard deviation of 1). In embodiments where the sensors of the accelerometer device have a different sensitivity to pressure, it is possible to take into account this different sensitivity from the error law due to the pressure and the positioning of the sensors. The accelerometer device 1 thus offers a low-cost solution for measuring the acceleration of an acoustic antenna and compensating the effect of the pressure. In some acoustic applications of the invention, it has been observed in particular that the accelerometer device can be used up to 100 Bars (1000m) with good resistance up to 500 Bars (5000m). The accelerometer device 1 also has a small footprint, which makes it possible to stack a plurality of cards 102 to ensure continuity of operation in case of failure. The accelerometer device also makes it possible to reduce the error rate of 20% observed with conventional accelerometer devices to a rate equal to 1%. It also allows a redundancy of values and therefore an improvement in reliability. The accelerometer device 1 also has good endurance and reliability over time. In particular, it has been observed that the pressure sensitivity of a MEMS sensor is constant over time, throughout the life of the device. The invention is not limited to the embodiments described above by way of non-limiting example. It encompasses all the embodiments that may be envisaged by those skilled in the art. In particular, the invention is not limited to a type of MEMS accelerometer sensor (11, 12). Nor is it limited to a number of accelerometer sensors or to a particular arrangement of the accelerometer device in an associated acoustic module. Furthermore, the calibration phase according to steps 900 and 901 may be omitted in certain embodiments or implemented differently.
    [0025] More generally, the invention is not limited to an application of the accelerometer device to a flute-type acoustic antenna and can be used to measure the 3-axis acceleration of any object to which it is mechanically connected. The invention can be used for example to remove right / left ambiguity underwater acoustic detection or to determine the direction of an object in space. In particular, the accelerometer device 1 can be used, for example, at a standstill for measuring terrestrial gravity in so-called "self test" mode. The output of the processing unit 15 may be used in particular by a positioning adjustment mechanism (not shown) to adjust the positioning of the object from the references calculated by the processing unit 15 along each axis, according to a servo loop.
    权利要求:
    Claims (13)
    [0001]
    REVENDICATIONS1. Accelerometer device for determining the acceleration of an object to which the accelerometer device is mechanically connected, along 3 X, Y and Z axes of a main orthonormal reference system (X, Y, Z) comprising three axes X, Y, Z said object being subjected to a surrounding pressure, characterized in that it comprises a number N of MEMS type accelerometer sensors (11, 12, 13), said number N of accelerometer sensors being at least two, each sensor (11, 12, 13) being defined by construction in an auxiliary reference system comprising 3 orthonormal axes (Xi, Yi, Zi), said set of accelerometer sensors comprising at least one pair of sensors mounted opposite head and substantially parallel to each other , and in that: - for each of said pairs of accelerometer sensors, the sensors have two-by-two components of opposite sign along two axes of the main reference system; and the axes of the reference system according to which the components of the accelerometer sensors are two to two opposite on all the pairs of sensors comprise at least two of the three axes X, Y and Z of the reference system, which makes it possible to compensate the effect of the pressure on at least two axes of the reference system.
    [0002]
    2. An accelerometer device according to claim 1, characterized in that it comprises a processing unit (15) for calculating the average of the acceleration along each axis X, Y and Z, the average of the accelerations along a given axis being determined from accelerations determined by each accelerometer sensor along said given axis.
    [0003]
    3. accelerometer device according to claim 2, characterized in that the calculation of the average accelerations along a given axis also takes into account the gain and / or the offset of each predetermined sensor in a unit calibration phase implemented separately. for each sensor before mounting.
    [0004]
    4. accelerometer device according to one of claims 1 and 2, characterized in that the calculation of the average accelerations along a given axis also takes into account a predefined gain compensation factor.
    [0005]
    5. An accelerometer device according to one of the preceding claims, characterized in that said set of sensors comprises two accelerometer sensors (11, 12) connected to at least one printed circuit board (102), and in that the axes of the reference system in which the sensor components are two to two opposite on the set of sensors comprise two of the three X, Y and Z axes of the reference system, which makes it possible to correct the effect of the pressure exerted on the object along both axes.
    [0006]
    6. accelerometer device according to one of claims 1 to 4, characterized in that said set of sensors accelerometers comprises three sensors (11, 12, 13), and in that the axes of the reference system according to which the components of the sensors are two to two opposite on all sensors include the three axes X, Y and Z of the reference system, which corrects the effect of the pressure exerted on the object along the three axes.
    [0007]
    7. accelerometer device according to one of the preceding claims, characterized in that said object is an acoustic antenna (10) comprising a set of multi acoustic sensors (101), each acoustic multi sensor (101) being mounted on at least a printed circuit board (102) and in that the accelerations determined by the accelerometer device along each axis X, Y and Z are used to compensate for the effect of the acceleration of the acoustic antenna (10) on the position multi acoustic sensor.
    [0008]
    8. accelerometer device according to one of the preceding claims, characterized in that the sensors have a different sensitivity to pressure.
    [0009]
    Acoustic antenna acoustic antenna module (10) extending along a main axis, characterized in that it comprises an accelerometer device (1) according to one of claims 1 to 8, and in that the determined accelerations by the accelerometer device along each axis X, Y and Z are used to compensate for the effect of the acceleration of the acoustic antenna (10) on the position of the multi acoustic sensor.
    [0010]
    10. Acoustic module according to claim 9, characterized in that the acoustic sensor (101) is a multi acoustic sensor axis substantially parallel to the axis of the antenna.
    [0011]
    11. Acoustic module according to one of claims 9 and 10, characterized in that it comprises at least one printed circuit board on which are mounted accelerometer sensors. 10
    [0012]
    12. Acoustic module according to claim 11, characterized in that it comprises a plurality of printed circuit boards (102), stacked substantially perpendicularly to the axis of the antenna, on which the accelerometer sensors are mounted.
    [0013]
    13. Antenna acoustic, characterized in that it comprises a set of 15 acoustic modules according to one of claims 9 to 12.
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    同族专利:
    公开号 | 公开日
    US20170205519A1|2017-07-20|
    SG11201700301YA|2017-02-27|
    AU2015289294A1|2017-02-02|
    CA2955213A1|2016-01-21|
    AU2015289294B2|2021-02-04|
    SG10201900320VA|2019-02-27|
    EP3170007B1|2020-05-20|
    EP3170007A1|2017-05-24|
    US10557952B2|2020-02-11|
    FR3023920B1|2018-01-05|
    WO2016008782A1|2016-01-21|
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    GB2581124B|2018-12-03|2021-08-11|Enteq Upstream Plc|Inclinometer|
    RU2717166C1|2019-06-13|2020-03-18|Федеральное Государственное Унитарное Предприятие "Всероссийский Научно-Исследовательский Институт Автоматики Им.Н.Л.Духова" |Three-component downhole seismic sensor|
    法律状态:
    2015-06-29| PLFP| Fee payment|Year of fee payment: 2 |
    2016-01-22| PLSC| Publication of the preliminary search report|Effective date: 20160122 |
    2016-06-28| PLFP| Fee payment|Year of fee payment: 3 |
    2017-06-28| PLFP| Fee payment|Year of fee payment: 4 |
    2018-06-28| PLFP| Fee payment|Year of fee payment: 5 |
    2020-06-25| PLFP| Fee payment|Year of fee payment: 7 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1401618A|FR3023920B1|2014-07-18|2014-07-18|ACCELEROMETER DEVICE|
    FR1401618|2014-07-18|FR1401618A| FR3023920B1|2014-07-18|2014-07-18|ACCELEROMETER DEVICE|
    PCT/EP2015/065589| WO2016008782A1|2014-07-18|2015-07-08|Accelerometer device|
    EP15736453.0A| EP3170007B1|2014-07-18|2015-07-08|Accelerometer device|
    AU2015289294A| AU2015289294B2|2014-07-18|2015-07-08|Accelerometer device|
    US15/325,041| US10557952B2|2014-07-18|2015-07-08|Accelerometer device|
    CA2955213A| CA2955213A1|2014-07-18|2015-07-08|Accelerometer device|
    SG11201700301YA| SG11201700301YA|2014-07-18|2015-07-08|Accelerometer device|
    SG10201900320VA| SG10201900320VA|2014-07-18|2015-07-08|Accelerometer device|
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