CIRCUIT AND METHOD FOR DRIVING A MICRO-ELECTRO-MECHANICAL RESONATOR OF A GYROSCOPE WITH A REDUCED EXCITATION OF SPURIOUS HARMONICS

    公开(公告)号:US20240240945A1

    公开(公告)日:2024-07-18

    申请号:US18403324

    申请日:2024-01-03

    CPC classification number: G01C19/5755

    Abstract: A driving circuit is implemented for a driving resonator stage of a MEMS gyroscope including at least a first and a second electrode and a movable mass The driving circuit includes a synchronization stage which receives an electrical position signal indicative of the position of the movable mass and generates a reference signal phase- and frequency-locked with the electrical position signal; a driving stage which generates, on the basis of the reference signal, a first and a second driving signal, which are applied to the first and, respectively, the second electrodes, so that the movable mass is subject to a first and a second electrostatic force which cause the movable mass to oscillate.

    MEMS DEVICE HAVING IMPROVED DETECTION PERFORMANCES

    公开(公告)号:US20240151741A1

    公开(公告)日:2024-05-09

    申请号:US18496653

    申请日:2023-10-27

    CPC classification number: G01P15/125 G01P2015/0882

    Abstract: The MEMS device is formed by a substrate and a movable structure suspended on the substrate. The movable structure has a first mass, a second mass and a first elastic group mechanically coupled between the first and the second masses. The first elastic group is compliant along a first direction. The first mass is configured to move with respect to the substrate along the first direction. The MEMS device also has a second elastic group mechanically coupled between the substrate and the movable structure and compliant along the first direction; and an anchoring control structure fixed to the substrate, capacitively coupled to the second mass and configured to exert an electrostatic force on the second mass along the first direction. The anchoring control structure controls the MEMS device in a first operating state, wherein the second mass is free to move with respect to the substrate along the first direction, and in a second operating state, wherein the anchoring control structure applies a pull-in force on the second mass which anchors the second mass to the anchoring structure.

    MICROELECTROMECHANICAL SENSOR DEVICE WITH ACTIVE OFFSET COMPENSATION

    公开(公告)号:US20240044932A1

    公开(公告)日:2024-02-08

    申请号:US18364847

    申请日:2023-08-03

    CPC classification number: G01P15/125

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

    MEMS INERTIAL SENSOR WITH HIGH RESISTANCE TO STICTION

    公开(公告)号:US20230184806A1

    公开(公告)日:2023-06-15

    申请号:US18147629

    申请日:2022-12-28

    CPC classification number: G01P15/125 G01P2015/0874

    Abstract: An inertial structure is elastically coupled through a first elastic structure to a supporting structure so as to move along a sensing axis as a function of a quantity to be detected. The inertial structure includes first and second inertial masses which are elastically coupled together by a second elastic structure to enable movement of the second inertial mass along the sensing axis. The first elastic structure has a lower elastic constant than the second elastic structure so that, in presence of the quantity to be detected, the inertial structure moves in a sensing direction until the first inertial mass stops against a stop structure and the second elastic mass can move further in the sensing direction. Once the quantity to be detected ends, the second inertial mass moves in a direction opposite to the sensing direction and detaches the first inertial mass from the stop structure.

    Z-AXIS MICROELECTROMECHANICAL SENSOR DEVICE WITH IMPROVED STRESS INSENSITIVITY

    公开(公告)号:US20230160921A1

    公开(公告)日:2023-05-25

    申请号:US18055804

    申请日:2022-11-15

    CPC classification number: G01P15/18 G01P15/125 G01P15/0802

    Abstract: A microelectromechanical sensor device has a detection structure, having: a substrate, with a top surface; an inertial mass, suspended above the top surface of the substrate and elastically coupled to a rotor anchor so as to perform an inertial movement relative to the substrate as a function of a quantity to be detected; and stator electrodes, integrally coupled to the substrate at respective stator anchors and capacitively coupled to the inertial mass so as to generate a differential capacitive variation in response to, and indicative of, the quantity to be detected. In particular, the inertial mass performs, as the inertial movement, a translation movement along a vertical axis orthogonal to the top surface of the substrate; and the stator electrodes are arranged in a suspended manner above the top surface of the substrate.

    MEMS INERTIAL SENSOR WITH HIGH RESILIENCE TO THE PHENOMENON OF STICTION

    公开(公告)号:US20230083632A1

    公开(公告)日:2023-03-16

    申请号:US18056203

    申请日:2022-11-16

    Abstract: A MEMS inertial sensor includes a supporting structure and an inertial structure. The inertial structure includes at least one inertial mass, an elastic structure, and a stopper structure. The elastic structure is mechanically coupled to the inertial mass and to the supporting structure so as to enable a movement of the inertial mass in a direction parallel to a first direction, when the supporting structure is subjected to an acceleration parallel to the first direction. The stopper structure is fixed with respect to the supporting structure and includes at least one primary stopper element and one secondary stopper element. If the acceleration exceeds a first threshold value, the inertial mass abuts against the primary stopper element and subsequently rotates about an axis of rotation defined by the primary stopper element. If the acceleration exceeds a second threshold value, rotation of the inertial mass terminates when the inertial mass abuts against the secondary stopper element.

    METHOD FOR CORRECTING GYROSCOPE DEMODULATION PHASE DRIFT

    公开(公告)号:US20230068616A1

    公开(公告)日:2023-03-02

    申请号:US17460030

    申请日:2021-08-27

    Abstract: A gyroscopic sensor unit detects a phase drift between a demodulated output signal and demodulation signal during output of a quadrature test signal. A delay calculator detects the phase drift based on changes in the demodulated output signal during application of the quadrature test signal. A delay compensation circuit compensates for the phase drift by delaying the demodulation signal by the phase drift value.

    MEMS ACTUATOR FOR IN-PLANE MOVEMENT OF A MOBILE MASS AND OPTICAL MODULE COMPRISING THE MEMS ACTUATOR

    公开(公告)号:US20220380199A1

    公开(公告)日:2022-12-01

    申请号:US17752016

    申请日:2022-05-24

    Abstract: A MEMS actuator includes a mobile mass suspended over a substrate in a first direction and extending in a plane that defines a second direction and a third direction perpendicular thereto. Elastic elements arranged between the substrate and the mobile mass have a first compliance in a direction parallel to the first direction that is lower than a second compliance in a direction parallel to the second direction. Piezoelectric actuation structures have a portion fixed with respect to the substrate and a portion that deforms in the first direction in response to an actuation voltage. Movement-transformation structures coupled to the piezoelectric actuation structures include an elastic movement-conversion structure arranged between the piezoelectric actuation structures and the mobile mass. The elastic movement-conversion structure is compliant in a plane formed by the first and second directions and has first and second principal axes of inertia transverse to the first and second directions.

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