A gyroscope includes a proof mass, and a first transduction/suspension structure coupled to the proof mass with a laterally flexible first coupling spring from a first coupling direction. A second transduction/suspension structure is coupled to the proof mass with a laterally flexible second coupling spring from a second coupling direction. A third transduction/suspension structure is coupled to the proof mass with a transversally flexible third coupling spring from a third coupling direction. A fourth transduction/suspension structure is coupled to the proof mass with a transversally flexible fourth coupling spring from a fourth coupling direction. Each transduction/suspension structure comprises elongated beams. Piezoelectric transducers are deposited on some elongated beams, and are configured to bend the corresponding elongated beams in the device plane and to measure the bending of the corresponding lateral elongated beams in the device plane.

A microelectromechanical system (MEMS) gyroscope includes a driving mass and a driving circuit that operates to drive the driving mass in a mechanical oscillation at a resonant drive frequency. An oscillator generates a system clock that is independent of and asynchronous to the resonant drive frequency. A clock generator circuit outputs a first clock and a second clock that are derived from the system clock. The drive loop of the driving circuit including an analog-to-digital converter (ADC) circuit that is clocked by the first clock and a digital signal processing (DSP) circuit that is clocked by the second clock.

A rotation rate sensor including a substrate, a drive structure, which is movable with regard to the substrate, a detection structure, and a Coriolis structure, the drive structure, the Coriolis structure, and the detection structure being essentially situated in a layer, in that an additional layer is situated essentially in parallel to the layer above or underneath the layer, a mechanical connection between the Coriolis structure and the drive structure being established with a first spring component, the first spring component being configured as a part of the additional layer, and/or a mechanical connection between the detection structure and the substrate being established with a second spring component, the second spring component being configured as a part of the additional layer.

A rotation rate sensor including a substrate, a drive structure, which is movable with regard to the substrate, a detection structure, and a Coriolis structure, the drive structure, the Coriolis structure, and the detection structure being essentially situated in a layer, in that an additional layer is situated essentially in parallel to the layer above or underneath the layer, a mechanical connection between the Coriolis structure and the drive structure being established with a first spring component, the first spring component being configured as a part of the additional layer, and/or a mechanical connection between the detection structure and the substrate being established with a second spring component, the second spring component being configured as a part of the additional layer.

A microelectromechanical gyroscope which comprises one or more Coriolis masses driven by a drive transducer and a force-feedback system. The force-feedback circuit comprises first and second sideband modulators and the self-test circuit comprises first and second sideband demodulators.

A microelectromechanical gyroscope which comprises one or more Coriolis masses driven by a drive transducer and a force-feedback system. The force-feedback circuit comprises first and second sideband modulators and the self-test circuit comprises first and second sideband demodulators.

A microelectromechanical system (MEMS) gyroscope includes a driving mass and a driving circuit that operates to drive the driving mass in a mechanical oscillation at a resonant drive frequency. An oscillator generates a system clock that is independent of and asynchronous to the resonant drive frequency. A clock generator circuit outputs a first clock and a second clock that are derived from the system clock. The drive loop of the driving circuit including an analog-to-digital converter (ADC) circuit that is clocked by the first clock and a digital signal processing (DSP) circuit that is clocked by the second clock.

A dynamically balanced 3-axis gyroscope architecture is provided. Various embodiments described herein can facilitate providing linear and angular momentum balanced 3-axis gyroscope architectures for better offset stability, vibration rejection, and lower part-to-part coupling.

A dynamically balanced 3-axis gyroscope architecture is provided. Various embodiments described herein can facilitate providing linear and angular momentum balanced 3-axis gyroscope architectures for better offset stability, vibration rejection, and lower part-to-part coupling.

A gyroscope includes a proof mass, and a first transduction/suspension structure coupled to the proof mass with a laterally flexible first coupling spring from a first coupling direction. A second transduction/suspension structure is coupled to the proof mass with a laterally flexible second coupling spring from a second coupling direction. A third transduction/suspension structure is coupled to the proof mass with a transversally flexible third coupling spring from a third coupling direction. A fourth transduction/suspension structure is coupled to the proof mass with a transversally flexible fourth coupling spring from a fourth coupling direction. Each transduction/suspension structure comprises elongated beams. Piezoelectric transducers are deposited on some elongated beams, and are configured to bend the corresponding elongated beams in the device plane and to measure the bending of the corresponding lateral elongated beams in the device plane.