Stmicroelectronics S.r.l.

Patrick Fedeli

Carlo Valzasina

Enri Duqi

Gabriele Gattere

Luca Giuseppe Falorni

Luca Guerinoni

Silvia Adorno

Giacomo Langfelder

Nicolo' Manca

Leonardo Gaffuri Pagani

Paola Carulli

Nicolò Manca

A method of determining calibrated values of atmospheric pressure using a reference value of atmospheric pressure and measured values of atmospheric pressure acquired when movable devices are and are not being inductively charged by a fixed device. An electronic apparatus having the fixed device and the movable devices having movable barometers.

Method for determining calibrated values of atmospheric pressure and related electronic apparatus

A microelectromechanical gyroscope is provided with a detection structure having: a substrate with a top surface parallel to a horizontal plane (xy); a mobile mass, suspended above the substrate to perform, as a function of a first angular velocity (Ω) around a first axis (x) of the horizontal plane (xy), at least a first detection movement of rotation around a second axis (y) of the horizontal plane; and a first and a second stator elements integral with the substrate and arranged underneath the mobile mass to define a capacitive coupling, a capacitance value thereof is indicative of the first angular velocity (Ω). The detection structure has a single mechanical anchorage structure for anchoring both the mobile mass and the stator elements to the substrate, arranged internally with respect to the mobile mass, which is coupled to this single mechanical anchorage structure by coupling elastic elements yielding to torsion around the second axis; the stator elements are integrally coupled to the single mechanical anchorage structure in an arrangement suspended above the top surface of the substrate.

Microelectromechanical gyroscope with out-of-plane detection movement

A microelectromechanical device includes a substrate, a first structural layer, and a second structural layer of semiconductor material. A sensing mass extends in the first structural layer and is coupled to the substrate by first elastic connections to enable oscillation of the sensing mass in a sensing direction perpendicular to the substrate by a maximum amount relative to a resting position of the sensing mass. An out-of-plane stopper structure includes an anchorage fixed to the substrate and a mechanical end-of-travel structure, which extends in the second structural layer, faces the sensing mass, and is separated therefrom by a gap having a width smaller than the maximum displacement distance of the sensing mass. The mechanical end-of-travel structure is coupled to the anchorage by second elastic connections that enable movement of the mechanical end-of-travel structure in the sensing direction in response to an impact of the sensing mass.

Microelectromechanical device with out-of-plane stopper structure

In an embodiment a circuit includes an inertial measurement unit configured to be oscillated via a driving signal provided by driving circuitry, a lock-in amplifier configured to receive a sensing signal from the inertial measurement unit and a reference demodulation signal which is a function of the driving signal and provide an inertial measurement signal based on the sensing signal, wherein the reference demodulation signal is affected by a variable phase error, phase meter circuitry configured to receive the driving signal and the sensing signal and provide, as a function of a phase difference between the driving signal and the sensing signal, a phase correction signal for the reference demodulation signal and a correction node configured to apply the phase correction signal to the reference demodulation signal so that, in response to the phase correction signal being applied to the reference demodulation signal, the phase error is maintained in a vicinity of a reference value.

Inertial measurement circuit, corresponding device and method

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Senago, Italy

Patrick Fedeli