FM INERTIAL SENSOR AND METHOD FOR OPERATING THE FM INERTIAL SENSOR

    公开(公告)号:US20190064205A1

    公开(公告)日:2019-02-28

    申请号:US16116467

    申请日:2018-08-29

    Abstract: An inertial sensor for sensing an external acceleration includes: a first and a second proof mass; a first and a second capacitor formed between first and second fixed electrodes and the first proof mass; a third and a fourth capacitor formed between third and fourth fixed electrodes and the second proof mass; a driving assembly configured to cause an antiphase oscillation of the first and second proof masses; a biasing circuit configured to bias the first and third capacitors, thus generating first variation of the oscillation frequency in a first time interval, and to bias the second and fourth capacitors, thus generating first variation of the oscillation frequency in a second time interval; a sensing assembly, configured to generate an differential output signal which is a function of a difference between a value of the oscillating frequency during the first time interval and a value of the oscillating frequency during the second time interval. Such differential output signal can be correlated to the value and direction of the external acceleration.

    MICROMECHANICAL DEVICE WITH ELASTIC ASSEMBLY HAVING VARIABLE ELASTIC CONSTANT

    公开(公告)号:US20230296643A1

    公开(公告)日:2023-09-21

    申请号:US18322488

    申请日:2023-05-23

    CPC classification number: G01P15/125

    Abstract: A micromechanical device includes a semiconductor body, a first mobile structure, an elastic assembly, coupled to the first mobile structure and to the semiconductor body and adapted to undergo deformation in a direction, and at least one abutment element. The elastic assembly is configured to enable an oscillation of the first mobile structure as a function of a force applied thereto. The first mobile structure, the abutment element and the elastic assembly are arranged with respect to one another in such a way that: when the force is lower than a force threshold, the elastic assembly operates with a first elastic constant; and when the force is greater than the threshold force, then the first mobile structure is in contact with the abutment element, and a deformation of the elastic assembly is generated, which operates with a second elastic constant different from the first elastic constant.

    WIDE BANDWIDTH MEMS ACCELEROMETER FOR DETECTING VIBRATIONS

    公开(公告)号:US20220033254A1

    公开(公告)日:2022-02-03

    申请号:US17385555

    申请日:2021-07-26

    Abstract: A MEMS accelerometer includes a supporting structure, at least one deformable group and one second deformable group, which include, respectively, a first deformable cantilever element and a second deformable cantilever element, which each have a respective first end, which is fixed to the supporting structure, and a respective second end. The first and second deformable groups further include, respectively, a first piezoelectric detection structure and a second piezoelectric detection structure. The MEMS accelerometer further includes: a first mobile mass and a second mobile mass, which are fixed, respectively, to the second ends of the first and second deformable cantilever elements and are vertically staggered with respect to the first and second deformable cantilever elements, respectively; and a first elastic structure, which elastically couples the first and second mobile masses.

    DUAL-MODE CONTROL CIRCUIT FOR MICROELECTROMECHANICAL SYSTEM GYROSCOPES

    公开(公告)号:US20240093995A1

    公开(公告)日:2024-03-21

    申请号:US17933743

    申请日:2022-09-20

    CPC classification number: G01C19/5712 H03F3/45475

    Abstract: The present disclosure is directed to a dual-mode control circuit for a microelectromechanical system (MEMS) gyroscope. A control circuit is coupled to a Lissajous frequency modulated (LFM) gyroscope to control amplitude of oscillation of a mass along two directions. The amplitude of oscillation is controlled by an automatic gain control (AGC) loop which allows the same amplitude of oscillation in both directions. An AGC is implemented with a combination of proportional control (P-type) and integral control (I-type) paths that maintain the correct Lissajous pattern of the oscillation of the mass. The AGC may include a dual-mode stage which is able to switch between a P-type control path and an I-type control path based on the operation of the LFM gyroscope. A fast start-up phase may be controlled by the P-type control path while the I-type path is pre-charged to be ready to use in a steady state condition.

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