A MEMS device may output a signal during operation that may include an in-phase component and a quadrature component. An external signal having a phase that corresponds to the quadrature component may be applied to the MEMS device, such that the MEMS device outputs a signal having a modified in-phase component and a modified quadrature component. A phase error for the MEMS device may be determined based on the modified in-phase component and the modified quadrature component.

A MEMS device may output a signal during operation that may include an in-phase component and a quadrature component. An external signal having a phase that corresponds to the quadrature component may be applied to the MEMS device, such that the MEMS device outputs a signal having a modified in-phase component and a modified quadrature component. A phase error for the MEMS device may be determined based on the modified in-phase component and the modified quadrature component.

A method of manufacturing a semiconductor device includes providing a semiconductor layer having a first-type region and a second-type region that are stacked and interface with each other to form a p-n junction, the first-type region defining a first side of the semiconductor layer and the second-type region defining a second side of the semiconductor layer. The method further includes providing an insulating layer on the second side of the semiconductor layer and etching the semiconductor layer from the first side of the semiconductor layer toward the second side of the semiconductor layer to form a trench. The first-type region corresponds to one of a n-type region and a p-type region, and the second-type region corresponds to the other of the n-type region and the p-type region.

A gyrometer including a first dual-mass gyrometer including a planar substrate, first left and right inertial masses including a first left and right frames, respectively, aligned along a first excitation axis X.sub.1 parallel to an excitation direction, and mounted with the ability to slide on the substrate along the first excitation axis X.sub.1, and first left and right central masses, respectively, mounted with the ability to slide in the first left and right frames, respectively, parallel to a first detection direction perpendicular to the excitation direction; a first coupling spring interposed between the first left and right frames; a first rocker mounted with the ability to rotate on the substrate about a first rocker pivot, first left and right ends of the first rocker being connected to the first left and right central masses, respectively; second left and right inertial masses aligned along a second axis X.sub.2 parallel to the excitation direction, and mounted with the ability to slide on the substrate along the second axis X.sub.2.

A vibrator device includes a vibrator element, and a support substrate disposed so as to be opposed to the vibrator element. The support substrate includes a base configured to support the vibrator element, a support configured to support the base, a plurality of beams configured to couple the base and the support to each other, and a drive signal interconnection, a drive constant-potential interconnection, a detection signal interconnection, and a detection constant-potential interconnection each laid around the base and the support passing the beams, and in predetermined one of the beams, at least one of the drive constant-potential interconnection and the detection constant-potential interconnection is disposed on a surface on the vibrator element side, and the detection signal interconnection is disposed on a surface on the opposite side.

A vibrator device includes a vibrator element, and a support substrate disposed so as to be opposed to the vibrator element. The support substrate includes a base configured to support the vibrator element, a support configured to support the base, a plurality of beams configured to couple the base and the support to each other, and a drive signal interconnection, a drive constant-potential interconnection, a detection signal interconnection, and a detection constant-potential interconnection each laid around the base and the support passing the beams, and in predetermined one of the beams, at least one of the drive constant-potential interconnection and the detection constant-potential interconnection is disposed on a surface on the vibrator element side, and the detection signal interconnection is disposed on a surface on the opposite side.

A gyroscope assembly includes a sense proof mass and a compensation proof mass. The sense proof mass has a sense frequency response in a sense dimension and is configured to move in a drive dimension in response to a drive signal, and to move in the sense dimension in response to experiencing an angular velocity about a sense input axis while moving in the drive dimension. And the compensation proof mass has, in the sense dimension, a compensation frequency response that is related to the sense frequency response.

An inertial sensor includes: a plurality of inertial force detection elements each configured to output an output signal corresponding to a detected inertial force; and a processor configured to execute processing relating to the output signal from each of the plurality of inertial force detection elements. The plurality of inertial force detection elements include a first inertial force detection element and a second inertial force detection element. A detection range of the first inertial force detection element and a detection range of the second inertial force detection element are different from each other. A sensitivity of the first inertial force detection element and a sensitivity of the second inertial force detection element are different from each other.

Angular sensor with vibrating resonator includes a supporting structure, a first mass and a second mass which are concentric, and mechanical springs arranged symmetrically in pairs, the pairs themselves being arranged symmetrically with respect to one another. Each spring comprises a first elastic leaf and a second elastic leaf which are connected to one another by one end, the first elastic leaf of one of the springs of each pair being parallel to the second elastic leaf of the other of the springs of the same pair. The four elastic leaves of at least one pair comprise two adjacent pairs of leaves making an angle of approximately 45° between them. The sensor is not provided with electrostatic springs.

A microelectromechanical system (MEMS) gyroscope sensor has a sensing mass and a quadrature error compensation control loop for applying a force to the sensing mass to cancel quadrature error. To detect fault, the quadrature error compensation control loop is opened and an additional force is applied to produce a physical displacement of the sensing mass. A quadrature error resulting from the physical displacement of the sensing mass in response to the applied additional force is sensed. The sensed quadrature error is compared to an expected value corresponding to the applied additional force and a fault alert is generated if the comparison is not satisfied.