Abstract: A device with a first MEMS device and a second MEMS device is disclosed. The first MEMS device is configured to sense at least one external influence. The second MEMS device is responsive to the at least one external influence. The first MEMS device is configured to change a state when the at least one external influence exceeds a threshold value. The first MEMS device is configured to retain the state below the threshold value, wherein the change in state of the first MEMS device is done passively and wherein the state of the first MEMS device is indicative of a status of the second MEMS device.

Abstract: A method and system for a sensor system of a device is disclosed. The sensor system includes a first MEMS sensor (FMEMS), a second MEMS sensor (SMEMS) and a signal processor (SP). An excitation is imparted to the device along a first axis (FA). The FMEMS has a first primary sense axis (FPSA), moves in response to a component of the excitation along the FA aligned with the FPSA and outputs a first signal proportional to an excitation along the FPSA. The SMEMS has a second primary sense axis (SPSA), moves in response to a component of the excitation along the FA aligned with the SPSA and outputs a second signal proportional to an excitation along the SPSA. The SP combines the first signal and the second signal to output a third signal proportional to the excitation along the FA. The FA, the FPSA and the SPSA have different orientations.

Abstract: A method includes receiving a signal from a sensor. The signal includes a first in-phase component and a first quadrature component. The first in-phase and quadrature components are identified. A rate signal is applied to the sensor and the sensor generates a sensed rate signal. A second in-phase and quadrature components associated with the sensed rate signal are determined. A phase error based on the first and the second in-phase components, and the first and the second quadrature components is determined. The method may further include reducing error in measurements associated with the sensor by dynamically compensating for the determined phase error, e.g., by modifying a clock signal, by changing a demodulation phase of a demodulator used to identify the in-phase and the quadrature components.

Abstract: A device comprising a micro-electro-mechanical system (MEMS) substrate with protrusions of different heights that has been integrated with a complementary metal-oxide-semiconductor (CMOS) substrate is presented herein. The MEMS substrate comprises defined protrusions of respective distinct heights from a surface of the MEMS substrate, and the MEMS substrate is bonded to the CMOS substrate. In an aspect, the defined protrusions can be formed from the MEMS substrate. In another aspect, the defined protrusions can be deposited on, or attached to, the MEMS substrate. In yet another aspect, the MEMS substrate comprises monocrystalline silicon and/or polysilicon. In yet even another aspect, the defined protrusions comprise respective electrodes of sensors of the device.

Abstract: A MEMS gyroscope includes a proof mass of a suspended spring mass system that is driven at a drive frequency. The proof mass moves relative to a sense electrode such that an overlap of the proof mass and sense electrode changes during the drive motion. A Coriolis force causes the proof mass to move relative to the sense electrode. The overlap and the movement due to the Coriolis force are sensed, and angular velocity is determined based on the magnitude of a signal generated due to a change in overlap and the Coriolis force.

Abstract: A device for reducing package stress sensitivity of a sensor includes one or more anchor points for attaching to a substrate; a rigid frame structure configured to at least partially support the sensor; and a compliant element between each anchor point and the rigid frame structure. Also disclosed is a device for supporting a micro-electro-mechanical (MEMS) sensor comprising four anchor points for attaching to a substrate; a rigid frame structure configured to support the MEMS sensor; and a crab-leg suspension element between each anchor point and the rigid frame structure, wherein the crab-leg suspension element is compliant. A method for reducing package stress sensitivity of a sensor is provided as well.

Abstract: A microelectromechanical system (MEMS) sensor includes a MEMS layer that includes fixed and movable electrodes. In response to an in-plane linear acceleration, the movable electrodes move with respect to the fixed electrodes, and acceleration is determined based on the resulting change in capacitance. A plurality of auxiliary electrodes are located on a substrate of the MEMS sensor and below the MEMS layer, such that a capacitance between the MEMS layer and the auxiliary loads changes in response to an out-of-plane movement of the MEMS layer or a portion thereof. The MEMS sensor compensates for the acceleration value based on the capacitance sensed by the auxiliary electrodes.

Abstract: 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.

Abstract: A method includes receiving a signal from a sensor. The signal includes a first in-phase component and a first quadrature component. The first in-phase and quadrature components are identified. A rate signal is applied to the sensor and the sensor generates a sensed rate signal. A second in-phase and quadrature components associated with the sensed rate signal are determined. A phase error based on the first and the second in-phase components, and the first and the second quadrature components is determined. The method may further include reducing error in measurements associated with the sensor by dynamically compensating for the determined phase error, e.g., by modifying a clock signal, by changing a demodulation phase of a demodulator used to identify the in-phase and the quadrature components.

Abstract: A method includes depositing a silicon layer over a first oxide layer that overlays a first silicon substrate. The method further includes depositing a second oxide layer over the silicon layer to form a composite substrate. The composite substrate is bonded to a second silicon substrate to form a micro-electro-mechanical system (MEMS) substrate. Holes within the second silicon substrate are formed by reaching the second oxide layer of the composite substrate. The method further includes removing a portion of the second oxide layer through the holes to release MEMS features. The MEMS substrate may be bonded to a CMOS substrate.

Abstract: Techniques for self-adjusting calibration of offset and sensitivity of a MEMS accelerometer are provided. In one example, a system comprises a first microelectromechanical (MEMS) sensor. The first MEMS sensor comprises: a proof mass coupled to an anchor connected to a reference plane, wherein the proof mass is coupled to the anchor via a first spring and a second spring; a plurality of reference paddles coupled to the anchor; and a plurality of acceleration sensing electrodes disposed on the reference plane, wherein a first area of each of the acceleration sensing electrodes is larger than a second area of each of a plurality of reference electrodes associated with the plurality of reference paddles.

Abstract: A MEMS sensor has a proof mass, a sense electrode, and a shield. At least a portion of the proof mass and shield may form a capacitor that causes an offset movement of the proof mass. A series of test values may be provided in order to minimize the offset movement or compensate for the offset movement. In some embodiments, the shield voltage may be modified to reduce the offset movement. Residual offsets due to other factors may also be determined and utilized for compensation to reduce an offset error in a sensed signal.

Abstract: In a first aspect, the angular rate sensor comprises a substrate and a rotating structure anchored to the substrate. The angular rate sensor also includes a drive mass anchored to the substrate and an element coupling the drive mass and the rotating structure. The angular rate sensor further includes an actuator for driving the drive mass into oscillation along a first axis in plane to the substrate and for driving the rotating structure into rotational oscillation around a second axis normal to the substrate; a first transducer to sense the motion of the rotating structure in response to a Coriolis force in a sense mode; and a second transducer to sense the motion of the sensor during a drive mode. In a second aspect the angular rate sensor comprises a substrate and two shear masses which are parallel to the substrate and anchored to the substrate via flexible elements. In further embodiments, a dynamically balanced 3-axis gyroscope architecture is provided.

Abstract: A MEMS capacitive sensing interface includes a sense capacitor having a first terminal and a second terminal, and having associated therewith a first electrostatic force. Further included in the MEMS capacitive sensing interface is a feedback capacitor having a third terminal and a fourth terminal, the feedback capacitor having associated therewith a second electrostatic force. The second and the fourth terminals are coupled to a common mass, and a net electrostatic force includes the first and second electrostatic forces acting on the common mass. Further, a capacitance measurement circuit measures the sense capacitance and couples the first terminal and the third terminal. The capacitance measurement circuit, the sense capacitor, and the feedback capacitor define a feedback loop that substantially eliminates dependence of the net electrostatic force on a position of the common mass.

Abstract: A system and method in accordance with an embodiment reduces the cross-axis sensitivity of a gyroscope. This is achieved by building a gyroscope using a mechanical transducer that comprises a spring system that is less sensitive to fabrication imperfection and optimized to minimize the response to the rotations other than the intended input rotation axis.

Abstract: Embodiments for modifying a spring mass configuration are disclosed that minimize the effects of unwanted nonlinear motion on a MEMS sensor. The modifications include any or any combination of providing a rigid element between rotating structures of the spring mass configuration, tuning a spring system between the rotating structures and coupling an electrical cancellation system to the rotating structures. In so doing unwanted nonlinear motion such as unwanted 2nd harmonic motion is minimized.

Abstract: Embodiments for modifying a spring mass configuration are disclosed that minimize the effects of unwanted nonlinear motion on a MEMS sensor. The modifications include any or any combination of providing a rigid element between rotating structures of the spring mass configuration, tuning a spring system between the rotating structures and coupling an electrical cancellation system to the rotating structures. In so doing unwanted nonlinear motion such as unwanted 2nd harmonic motion is minimized.

Abstract: A system and method in accordance with an embodiment reduces the cross-axis sensitivity of a gyroscope. This is achieved by building a gyroscope using a mechanical transducer that comprises a spring system that is less sensitive to fabrication imperfection and optimized to minimize the response to the rotations other than the intended input rotation axis. The longitudinal axes of the first and second flexible elements are parallel to each other and parallel to the first direction.

Abstract: In a first aspect, the angular rate sensor comprises a substrate and a rotating structure anchored to the substrate. The angular rate sensor also includes a drive mass anchored to the substrate and an element coupling the drive mass and the rotating structure. The angular rate sensor further includes an actuator for driving the drive mass into oscillation along a first axis in plane to the substrate and for driving the rotating structure into rotational oscillation around a second axis normal to the substrate; a first transducer to sense the motion of the rotating structure in response to a Coriolis force in a sense mode; and a second transducer to sense the motion of the sensor during a drive mode. In a second aspect the angular rate sensor comprises a substrate and two shear masses which are parallel to the substrate and anchored to the substrate via flexible elements.

Abstract: A system and/or method for utilizing MEMS switching technology to operate MEMS sensors. As a non-limiting example, a MEMS switch may be utilized to control DC and/or AC bias applied to MEMS sensor structures. Also for example, one or more MEMS switches may be utilized to provide drive signals to MEMS sensors (e.g., to provide a drive signal to a MEMS gyroscope).