Patent Description:
MEMS accelerometers are known having a sensing axis in the horizontal plane, i.e. including sensing structures sensitive to accelerations acting along at least one direction parallel to a corresponding plane of main extension and to a top surface of a corresponding substrate of semiconductor material; MEMS accelerometers are also known with vertical sensing axis, i.e. including sensing structures sensitive to accelerations acting along a direction orthogonal to the same plane of main extension.

In general, the sensing structure of a MEMS accelerometer comprises at least one mobile mass moving due to inertial effect, generally defined as "rotor mass" or simply "rotor" as it is movable due to the inertial effect (without this however implying for the same inertial mass to necessarily have a rotational movement) in the presence of an acceleration to be sensed, and mobile electrodes (or rotor electrodes) integrally coupled thereto.

The rotor mass is arranged suspended above a substrate, coupled to a corresponding rotor anchoring structure (integral with the same substrate) by means of coupling elastic elements, which allow its movement due to the inertial effect along one or more sensing directions.

The sensing structure of the MEMS accelerometer also comprises fixed or stator electrodes, integrally coupled to the substrate by respective stator anchors, capacitively coupled to the rotor electrodes to form sensing capacitors, having a sensing capacitance indicative of the quantity to be sensed.

Typically, the stator electrodes are divided into two groups, the electrodes of each group being biased to a different biasing voltage and being arranged facing respective rotor electrodes to have opposite variations of a facing distance (and, consequently, of a sensing capacitance) due to the inertial movement of the rotor mass, so as to implement a differential configuration.

The MEMS accelerometer also comprises an electronic circuit (so-called ASIC - Application Specific Integrated Circuit), electrically coupled to the sensing structure, which receives at input the capacitive variations produced by the sensing capacitors and processes them to determine the acceleration value, for generation of an output electrical signal (which may be provided externally to the MEMS accelerometer for further processing).

The aforementioned ASIC electronic circuit and the sensing structure are typically provided in respective dies of semiconductor material, which are enclosed within a housing, so-called package, which encloses and protects the same dies, also providing an electrical connection interface towards the outside; in so-called substrate-level package solutions, the package is formed by one or more base and cap layers, which are directly coupled to the dies of the MEMS device, forming their mechanical and electrical interfaces towards the external environment.

A known problem affecting the sensing structures of known MEMS accelerometers is represented by the so-called offset error, that is, by a non-zero value of the output signal in the absence of an acceleration to be sensed.

The offset error is due to the fact that the rotor mass and the associated rotor electrodes, in neutral or rest condition (i.e. in the aforementioned condition of absence-of-acceleration), are not centered (not equidistant) with respect to the stator electrodes; this error is therefore intrinsic to the manufacturing of the MEMS accelerometer sensing structure.

In particular, the offset of the rotor mass is typically due to a residual manufacturing stress affecting the material, typically polycrystalline silicon, forming the aforementioned coupling elastic elements that couple the rotor mass to the corresponding anchoring structure. The offset may be considered as a force acting on the coupling elastic elements, determining a deformation thereof that is present even in the aforementioned rest condition.

The offset generally creates a mismatch of the sensing capacitance (and sensitivity) values between the rotor electrodes and the stator electrodes of the two groups in the aforementioned differential configuration. As a result, an increase occurs in the non-linearity and the so-called VRE (Vibration Rectification Error) error (that is associated with the response of the accelerometer to AC vibrations which are rectified, showing up as an anomalous shift in the offset of the accelerometer).

In particular, the non-linear relationship between the capacitance and the displacement between the rotor and stator electrodes entails an asymmetry in the ΔC/Δg characteristic in the presence of an initial offset (where C represents the capacitance and g the acceleration); in other words, a positive displacement between the electrodes results, for example, in a greater capacitive variation with respect to a negative displacement.

Furthermore, a reduction of the full-scale value of the MEMS accelerometer occurs. In particular, the presence of an initial offset significantly reduces the full scale, by reducing the range of the displacement of the electrodes (before reaching corresponding stop elements, so-called stoppers).

High-end applications, such as for example structural analysis or vibrational monitoring applications of the condition of mechanical elements, require high performances by the MEMS accelerometers; as a result, the aforementioned problems linked to the intrinsic offset of the same MEMS accelerometers may not be acceptable.

A solution that has been proposed to overcome these drawbacks provides for a suitable electronic compensation, for example in the associated ASIC electronic circuit, using a compensation capacitance, of a suitable value, which is coupled in parallel to the sensing capacitances, to obtain at output a compensated signal. However, the working point of the MEMS accelerometer remains affected by the offset intrinsic to the sensing structure, with the resulting previously discussed problems of non-linearity and sensitivity and full-scale value reduction.

<CIT> discloses a sensing system for a micromechanical sensor device, comprising: a seismic mass that can be moved along a sensing direction; and at least one sensing element arranged on one side of the seismic mass at an orthogonal angle to the sensing direction. The system is characterized in that at least one comb electrode is arranged on each opposite side of the seismic mass at an orthogonal angle to the sensing element and a respective constant electrical compensation voltage can be supplied to each of the at least two comb electrodes in order to compensate for a mechanical offsetting of the sensing element.

The aim of the present solution is therefore to provide a microelectromechanical sensor device, in particular an accelerometer, which allows the previously highlighted problems to be overcome.

According to the present solution, a microelectromechanical sensor device is provided, as defined in the attached claims.

For a better understanding of the present invention, preferred embodiments thereof are now described, purely by way of non-limiting example, with reference to the attached drawings, wherein:.

As will be described in detail, one aspect of the present solution provides for the introduction, in the sensing structure of a microelectromechanical sensor device, in particular of a MEMS accelerometer having an inertial mass, of stator electrodes which may be moved relative to respective rotor electrodes associated with the inertial mass.

In this manner it is possible to carry out an active offset compensation, moving the stator electrodes, in this case movable and repositionable, so that they are substantially equidistant with respect to the respective rotor electrodes (despite a possible native displacement of the rotor mass, for example due to residual stress of corresponding coupling elastic elements). The position of the same stator electrodes, on the other hand, remains fixed with respect to the quantity to be sensed, in such a way as not to alter the sensing characteristics of the sensor device.

<FIG> shows a sensing structure <NUM> of a microelectromechanical sensor device, in particular a MEMS accelerometer with a sensing axis in the horizontal plane, according to an aspect of the present solution.

The sensing structure <NUM> comprises: a substrate <NUM> of semiconductor material, for example silicon, having a top surface extending into a horizontal plane xy, defined by a first and a second horizontal axes x, y orthogonal to each other; and an inertial mass <NUM>, formed by conductive material, for example suitably doped epitaxial silicon, and arranged above the substrate <NUM>, suspended at a certain distance from its top surface.

The inertial mass <NUM> is also customarily referred to as "rotor mass" or simply "rotor", as it is movable due to inertial effect, without this implying, however, that the same inertial mass <NUM> has a rotational movement; as described below, in this embodiment, the inertial mass <NUM> has, conversely, a linear movement in response to sensing of an acceleration along a sensing axis.

The inertial mass <NUM> has a main extension in the horizontal plane xy, parallel to the top surface of the substrate <NUM>, and a substantially negligible dimension along an orthogonal axis z, perpendicular to the aforementioned horizontal plane xy and forming with the first and the second horizontal axes x, y a set of three Cartesian axes xyz. In particular, the second horizontal axis y coincides in this case with the sensing axis of the sensing structure <NUM>.

The inertial mass <NUM> has the shape of a frame, for example substantially square or rectangular (or, in other words, of a square or rectangular ring), in the aforementioned horizontal plane xy and has centrally a through opening, defining a window <NUM>, traversing it throughout an entire thickness thereof.

The sensing structure <NUM> further comprises a rotor anchoring structure <NUM>, arranged centrally within the window <NUM> and integrally coupled to the top surface of the substrate <NUM>. In the illustrated embodiment, this rotor anchoring structure <NUM> comprises a first and a second rotor anchoring element 7a, 7b, having a substantially rectangular shape in the horizontal plane xy and, in the illustrated example, longitudinal extension along the second horizontal axis y. Each of these first and second rotor anchoring elements 7a, 7b is integrally coupled to the substrate <NUM> by a coupling portion, which extends for example as a pillar between the top surface of the substrate <NUM> and the anchoring structure <NUM>.

The inertial mass <NUM> is elastically coupled to the rotor anchoring structure <NUM> by elastic coupling elements <NUM>, arranged within the window <NUM> between the same inertial mass <NUM> and the rotor anchoring structure <NUM>, on opposite sides of the same rotor anchoring structure <NUM>, in the direction of the second horizontal axis y.

In the illustrated embodiment, a first elastic coupling element 8a, of a folded type, couples the first rotor anchoring element 7a to a first side (e.g., a short side) of the frame of the inertial mass <NUM>; and a second elastic coupling element 8b, also of a folded type, couples the second rotor anchoring element 7b to a second side (opposite to the first side along the second horizontal axis y) of the same frame of the inertial mass <NUM>.

In particular, the elastic coupling elements <NUM> are configured to allow movement of the inertial mass <NUM> along the second horizontal axis y with respect to the substrate <NUM>, being yielding to deformations along the same second horizontal axis y (being substantially rigid with respect to deformations along different directions in the horizontal plane xy or transverse to the same horizontal plane xy).

The inertial mass <NUM> also carries a certain number of rotor electrodes <NUM>, integrally coupled to the same inertial mass <NUM> (being integral or "monolithic" with this inertial mass <NUM>), in the illustrated embodiment arranged externally to the frame and the corresponding window <NUM>. The aforementioned rotor electrodes <NUM> have a rectangular shape in the horizontal plane xy and, as well as the inertial mass <NUM>, are suspended above the substrate <NUM>, parallel to the top surface of the same substrate <NUM>.

In detail, in the illustrated embodiment, the aforementioned frame of the inertial mass <NUM> has centrally, at corresponding sides (e.g., long sides) extending along the second horizontal axis y, a first and a second recesses (or grooves) 10a, 10b.

The aforementioned rotor electrodes <NUM> comprise a first group of rotor electrodes 9a, which extend longitudinally along the first horizontal axis x within the first recess 10a, starting from the frame of the inertial mass <NUM>; and a second group of rotor electrodes 9b, which extend longitudinally along the first horizontal axis x within the second recess 10b, starting from the frame of the inertial mass <NUM>, in a symmetrical position and specular to the rotor electrodes 9a of the first group with respect to the second horizontal axis y (being aligned with each other along the first horizontal axis x).

The sensing structure <NUM> also comprises a certain number of stator electrodes <NUM>, facing respective rotor electrodes <NUM>, also having in the example a rectangular shape in the horizontal plane xy elongated along the first horizontal axis x.

According to an aspect of the present solution, these stator electrodes <NUM> are suspended above the substrate <NUM>, parallel to the top surface of the same substrate <NUM>; in other words, these stator electrodes <NUM> are not integrally coupled to the substrate <NUM>, but are suspended in a floating manner with respect to the same substrate <NUM>.

A first group of stator electrodes 12a are arranged within the first recess 10a, in a position facing and interdigitated with the rotor electrodes 9a of the first group, in particular being arranged on a first side of the second horizontal axis y with respect to the same rotor electrodes 9a. Correspondingly, a second group of stator electrodes 12b are arranged within the second recess 10b, in a position facing and interdigitated with the rotor electrodes 9b of the second group, in particular being arranged on a second side of the second horizontal axis y (opposite to the aforementioned first side) with respect to the same rotor electrodes 9b.

Essentially, a displacement of the inertial mass <NUM> along the second horizontal axis y causes a relative movement of the rotor electrodes 9a away from the stator electrodes 12a of the first group (and a corresponding decrease of a first sensing capacitance formed between the same electrodes); and a corresponding relative movement of the rotor electrodes 9b towards the stator electrodes 12b of the second group (and a corresponding increase of a second sensing capacitance formed between the same electrodes).

Ideally, in the absence of an external acceleration to be sensed (in the example, along the second horizontal axis y), the rotor electrodes 9a and the stator electrodes 12a of the first group have a facing distance from each other which is equal to a respective facing distance between the rotor electrodes 9b and the stator electrodes 12b of the second group (essentially, the rotor electrodes <NUM> are equidistant from the stator electrodes <NUM>).

However, as previously indicated, the inertial mass <NUM> may have, for example due to the presence of different residual stresses in the elastic coupling elements 8a, 8b, a native (undesired) displacement along the second axis y in a rest condition (e.g. in the direction indicated by the arrow in <FIG>), causing a mismatch between the aforementioned facing distances between the rotor electrodes 9a and the stator electrodes 12a of the first group and between the rotor electrodes 9b and the stator electrodes 12b of the second group.

Essentially, an initial variation occurs, in the rest condition, between the aforementioned first and second sensing capacitances with a resulting offset in the output signal; this offset is intrinsic or native to the sensing structure <NUM>.

According to an aspect of the present solution, the sensing structure <NUM> therefore comprises a compensation structure <NUM> (schematically shown in <FIG>) coupled to the stator electrodes <NUM> and configured to cause a suitable displacement thereof, in the example along the second horizontal axis y, in order to compensate for the aforementioned undesired initial displacement of the inertial mass <NUM> and, therefore, compensate the offset of the output signal.

In other words, the compensation structure <NUM> is operable to restore a situation of equidistance in the facing between the rotor electrodes 9a and the stator electrodes 12a of the first group and between the rotor electrodes 9b and the stator electrodes 12b of the second group.

As will be discussed below, the compensation structure <NUM> is coupled to the stator electrodes <NUM> in such a way that the same stator electrodes <NUM> are insensitive to the acceleration to be sensed (in the example the linear acceleration along the second horizontal axis y), thus behaving effectively as "fixed" or reference electrodes with respect to the rotor electrodes <NUM>, for sensing the same acceleration.

In detail, and with reference to <FIG>, a possible embodiment of the aforementioned compensation structure <NUM> is now described.

In this embodiment, the compensation structure <NUM> provides, for each group of stator electrodes 12a, 12b, a respective actuation structure <NUM>, with pivoting movement about a respective rotation axis A, B parallel to the orthogonal axis z, which comprises: a central pivot element <NUM>, anchored to the substrate <NUM>; a first arm <NUM>, coupled to the central pivot element <NUM> on a first side with respect to the first horizontal axis x by a rigid connection element <NUM> and carrying the stator electrodes 12a, 12b of the respective first or second group; and a second arm <NUM>, coupled to the central pivot element <NUM> by a respective rigid connection element <NUM> on a second side with respect to the first horizontal axis x, opposite to the first side, and carrying respective movable actuation electrodes <NUM>.

In the example illustrated in <FIG>, the aforementioned first and second arms <NUM>, <NUM> have a substantially rectangular shape in the horizontal plane xy, with extension along the second horizontal axis y and carry the respective stator electrodes 12a, 12b, respectively movable actuation electrodes <NUM>, at a side opposite to the central pivot element <NUM> with respect to the first horizontal axis x, with a rake- or fork-like arrangement.

The aforementioned central pivot element <NUM>, in the illustrated embodiment, comprises a frame <NUM>, substantially square in the horizontal plane xy, suspended above the substrate <NUM> and internally defining a window <NUM>; the frame <NUM> is coupled to a central anchor <NUM>, arranged centrally to the window <NUM> at the respective rotation axis A, B and integral with the substrate <NUM> (having for example a substantially vertical pillar shape).

In particular, the frame <NUM> is elastically coupled to the central anchor <NUM> by four coupling elastic elements <NUM>, arranged as a cross with respect to the aforementioned central anchor <NUM> and aligned in pairs along the first or second horizontal axes x, y; these coupling elastic elements <NUM> are yielding to bending in the horizontal plane xy, allowing the rotation of the frame <NUM> about the central anchor <NUM> and the respective rotation axis A, B.

The compensation structure <NUM> also comprises fixed actuation electrodes <NUM>, arranged in an interdigitated manner with the movable actuation electrodes <NUM> of a respective actuation structure <NUM> and anchored to the substrate <NUM> by a respective anchoring portion <NUM> (having for example a vertical columnar shape).

In the embodiment of <FIG>, the aforementioned fixed actuation electrodes <NUM> comprise first and second fixed actuation electrodes 35a, 35b, designed to be biased at a different biasing voltage, arranged on opposite sides of a respective movable actuation electrode <NUM> with respect to the second horizontal axis y.

During operation, a suitable biasing of the fixed actuation electrodes <NUM> with respect to the actuation structure <NUM> (which may be set to a reference voltage, for example about half of the dynamics of a corresponding reading electronics, for example about <NUM> V - <NUM> V) causes the displacement of the movable actuation electrodes <NUM> of the respective actuation structure <NUM> (e.g. in the direction of the second horizontal axis y, as indicated by the arrow in the same <FIG>), the resulting rotation of the central pivot element <NUM> about the central anchor <NUM> and the respective rotation axis A, B and the displacement (in the opposite directions of the same second horizontal axis y, again as indicated by the arrow in the same <FIG>) of the stator electrodes 12a, 12b of the respective first or second group.

This displacement of the stator electrodes 12a, 12b allows the desired mechanical offset compensation, canceling the effect of the native displacement of the inertial mass <NUM> and the associated capacitive mismatch between stator electrodes <NUM> and respective rotor electrodes <NUM>.

An offset compensation procedure may therefore be implemented which may provide, in the absence of external acceleration stimuli, for a process, for example an iterative process, of applying a suitable biasing voltage to the fixed actuation electrodes <NUM> of the compensation structure <NUM> for the resulting repositioning of the stator electrodes <NUM> with respect to the rotor electrodes <NUM>, until an offset-free output signal is obtained.

This offset compensation procedure may be performed at a first use of the MEMS accelerometer or at the start-up of the same MEMS accelerometer or, in any case, when it is deemed suitable (e.g. following the determination of an offset on the output signal greater than a certain threshold). Typically, the offset compensation procedure may be performed during a calibration executed at the end of the manufacturing process or after mounting on a printed circuit.

In a possible implementation, the aforementioned offset compensation procedure may be implemented by the ASIC electronic circuit of the MEMS accelerometer, or internally to the same MEMS accelerometer; alternatively, this procedure may be implemented externally to the MEMS accelerometer, for example by a control unit of an electronic device wherein the same MEMS accelerometer is used (in this case, this control unit providing suitable control and/or biasing signals to the MEMS accelerometer).

Advantageously, the aforementioned compensation structure <NUM> is insensitive to the external acceleration that needs to be sensed by the sensing structure <NUM>; in other words, in the example, the aforementioned compensation structure <NUM> is capable of rejecting the linear acceleration along the second horizontal axis y.

In particular, the aforementioned actuation structure <NUM>, being balanced with respect to the central pivot element <NUM>, does not move in the presence of a linear acceleration, acting along the second horizontal axis y; this acceleration in fact acts in a corresponding manner on the stator electrodes <NUM> and on the movable actuation electrodes <NUM>, on the opposite sides of the same central pivot element <NUM>, which therefore does not move and does not rotate about the central anchor <NUM>.

<FIG> shows a variant embodiment of the compensation structure <NUM> of the sensing structure <NUM> (generally having the same configuration shown in <FIG>).

In this variant, the fixed actuation electrodes <NUM> of the compensation structure <NUM> comprise only the first fixed actuation electrodes 35a (or, similarly and in a manner illustrated in this <FIG>, only the second fixed actuation electrodes 35b).

As previously illustrated, also in this embodiment the biasing of the fixed actuation electrodes <NUM> allows the offset to be compensated, in particular by compensating for the initial displacement of the inertial mass <NUM> due to the intrinsic or native offset.

However, since in this case it would be possible to move the stator electrodes <NUM> in only one direction of the second horizontal axis y (given the presence of only the first, or second, fixed actuation electrodes 35a, 35b), a specific biasing strategy of the same fixed actuation electrodes <NUM> is implemented.

In detail, the position of the fixed actuation electrodes <NUM> with respect to the movable actuation electrodes <NUM> is set (by a specific shape of the photolithographic masks during the formation of the compensation structure <NUM>) in such a way that, in the absence of external stimuli, the offset compensation occurs with a biasing voltage roughly corresponding to half of the biasing dynamics (for example, roughly about <NUM> V, in case the output dynamics is comprised between <NUM> and <NUM> V).

Using this particular biasing strategy, the two halves of the dynamics of the biasing voltage may be used to move the movable compensation electrodes <NUM> in opposite directions of the second horizontal axis y to compensate for displacements of the inertial mass <NUM> in both the aforementioned directions.

With reference to <FIG>, a further embodiment of the sensing structure <NUM> is now described, in this case for providing a MEMS accelerometer with an out-of-plane sensing axis (z axis).

As will be described in greater detail, in a manner similar to what has been previously described, the compensation structure <NUM> is again provided, configured to mechanically compensate for native displacements of the inertial mass <NUM> and, therefore, to compensate the offset of the output signal.

In detail, the inertial mass <NUM> is in this case coupled to the rotor anchoring structure <NUM>, arranged centrally within the window <NUM>, by elastic coupling elements 8a, 8b, yielding to torsion about a rotation axis parallel to the second horizontal axis y and defined by their longitudinal extension.

The same inertial mass <NUM> has an asymmetrical mass distribution with respect to this rotation axis, in such a way as to be set to rotation due to inertial effect in response to an acceleration to be sensed along the orthogonal axis z.

The rotor electrodes <NUM>, integrally coupled to the same inertial mass <NUM>, comprise in this case a first and a second rotor electrode 9a, 9b arranged on opposite sides with respect to the rotation axis and the rotor anchoring structure <NUM>, in a suspended manner above the substrate <NUM>. The first and second rotor electrodes 9a, 9b have a substantially rectangular shape in the horizontal plane xy, are arranged centrally with respect to the window <NUM> and are coupled to the frame of the inertial mass <NUM> by respective rigid connection elements <NUM> extending parallel to the second horizontal axis y, on opposite sides with respect to the respective rotor electrode 9a, 9b.

In this embodiment, the stator electrodes <NUM> are suspended again in a floating manner with respect to the substrate <NUM> (decoupled from the same substrate <NUM>), being in this case arranged in the window <NUM>, partially above the rotor electrodes <NUM>.

These stator electrodes <NUM> comprise herein a first stator electrode 12a, suspended above the first rotor electrode 9a; and a second stator electrode 12b, suspended above the second rotor electrode 9b. The aforementioned stator electrodes <NUM> have a substantially rectangular shape in the horizontal plane xy, with a greater extension with respect to the rotor electrodes <NUM>. In particular, these stator electrodes 12a, 12b have an overlap portion superimposed on the respective rotor electrode 9a, 9b only at a first half, closer to the rotation axis of the inertial mass <NUM>.

According to an aspect of the present solution, as shown schematically in <FIG>, in this case the actuation structure <NUM> of the compensation structure <NUM> is configured to constrain the same stator electrodes <NUM> in a pivoting manner about a respective constraint or central pivot element <NUM>, arranged centrally with respect to their extension in the horizontal plane xy and anchored to the substrate <NUM>, and about a respective rotation axis A, B.

In this case, the compensation structure <NUM> comprises fixed actuation electrodes <NUM>, arranged within the window <NUM>, below the stator electrodes <NUM>. In particular, these fixed actuation electrodes <NUM> comprise, for each stator electrode <NUM>, a pair of first and second fixed actuation electrodes 35a, 35b, arranged on opposite sides of the respective rotation axis A, B, below respective end portions of the respective stator electrode <NUM> and designed to be biased at a different biasing voltage.

During operation, the acceleration to be sensed along the orthogonal axis z causes a rotation of the inertial mass <NUM> and a differential variation of the sensing capacitances between the first rotor electrode 9a and the first stator electrode 12a and between the second rotor electrode 9b and the second stator electrode 12b.

During an offset compensation procedure, a suitable biasing of the fixed actuation electrodes <NUM> causes the rotation of the same stator electrodes <NUM> about the respective rotation axis A, B and a resulting variation of the facing distance with respect to the movable electrodes <NUM> and of the corresponding sensing capacitance.

Advantageously, also in this case, it is thus possible to compensate for the undesired displacement of the inertial mass <NUM> due, for example, to residual stresses in the elastic coupling elements <NUM>, and, therefore, to compensate the offset of the output signal.

Also in this case, the compensation structure <NUM> is insensitive to the acceleration to be sensed. In particular, given the symmetrical and balanced configuration with respect to the respective central constraint and the respective rotation axis A, B, the fixed electrodes <NUM> do not move in the presence of an acceleration to be sensed along the orthogonal axis z, thus not altering the sensing characteristics of the same acceleration.

The aforementioned sensing structure <NUM> may be advantageously formed using known processes of surface micromachining of semiconductor materials, for example by using the so-called double ThELMA (Thick Epipoly Layer for Microactuators and Accelerometers) process.

In general, the ThELMA process allows providing suspended structures with relatively small thickness (e.g. of the order of <NUM>-<NUM>), anchored to a substrate through yielding parts (springs) and therefore capable of moving, for example due to inertial effect, with respect to the underlying silicon substrate. The process consists in different production steps, including:.

In particular, for providing the sensing structure <NUM>, a double ThELMA process may be conveniently carried out, with the epitaxial growth of a further structural layer above the first structural layer provided epitaxially on the substrate.

In this case, the aforementioned stator electrodes <NUM> may be formed in the aforementioned further structural layer, suspended above the movable electrodes <NUM>, the latter being formed in the first structural layer.

The advantages of the present solution are clear from the previous description.

In any case, it is again underlined that the compensation structure <NUM> allows the non-linearity problems and the full-scale limitations associated with the intrinsic or natural offset to be solved, internally to the sensing structure <NUM> of the MEMS accelerometer (in particular, without requiring the presence of external electronics).

Furthermore, advantageously, this compensation structure <NUM> does not alter the motion, the equilibrium and stability of the same sensing structure <NUM>.

In this regard, it is highlighted that the fact that the actuation electrodes of the aforementioned compensation structure <NUM> do not face directly the inertial mass <NUM> avoids problems linked to possible electric fields due to electrostatic actuation (such as pull-in effects or changes in sensitivity or stability).

Finally, it is clear that modifications and variations may be made to what has been described and illustrated without thereby departing from the scope of the present invention, as defined in the attached claims.

In particular, it is underlined that a different solution to make the compensation structure <NUM> insensitive to the external acceleration that needs to be sensed by the sensing structure <NUM> may provide for designing the same compensation structure <NUM> with a resonance frequency much higher than that of the same sensing structure <NUM> (e.g., equal to <NUM>, against <NUM> of the sensing structure <NUM>).

Claim 1:
A microelectromechanical sensor device having a sensing structure (<NUM>) comprising:
a substrate (<NUM>);
an inertial mass (<NUM>), suspended above the substrate (<NUM>) and elastically coupled to an anchoring structure (<NUM>) by elastic coupling elements (<NUM>), so as to perform at least one inertial movement due to a quantity to be sensed;
first sensing electrodes (<NUM>), integrally coupled to the inertial mass (<NUM>) to be movable due to said inertial movement;
second sensing electrodes (<NUM>), fixed with respect to said quantity to be sensed, facing and capacitively coupled to the first sensing electrodes (<NUM>) to form sensing capacitances having a value indicative of the quantity to be sensed, wherein said second sensing electrodes (<NUM>) are arranged in a suspended manner above the substrate (<NUM>); and
a compensation structure (<NUM>),
characterized in that said compensation structure (<NUM>) is configured to move said second sensing electrodes (<NUM>) with respect to said first sensing electrodes (<NUM>) and vary a facing distance thereof, in the absence of said quantity to be sensed, in order to compensate for an offset of said sensing structure (<NUM>).