Abstract: A Micro-Electro-Mechanical Systems (MEMS) inertial sensor systems and methods determine linear acceleration and rotation in the in-pane and out-of-plane directions of the MEMS inertial sensor. An out-of-plane linear acceleration of the MEMS sensor may be sensed with the first out-of-plane electrode pair and the second out-of-plane electrode pair. An in-plane rotation of the MEMS sensor may be sensed with the first out-of-plane electrode pair and the second out-of-plane electrode. An in-plane linear acceleration of the MEMS sensor may be sensed with the first in-plane sense comb and the second in-plane sense comb. An out-of-plane rotation of the MEMS sensor may be sensed with the first in-plane sense comb and the second in-plane sense comb.

Abstract: A MEMS device (20) includes a substrate (22), a proof mass (28), and a frame structure (30) laterally spaced apart from the proof mass (28). Compliant members (36) are coupled to the proof mass (28) and the frame structure (30) to retain the proof mass (28) suspended above the surface (26) of the substrate (22) without directly coupling the proof mass (28) to the substrate (22). Anchors (32) suspend the frame structure (30) above the surface (26) of the substrate (22) without directly coupling the structure (30) to the substrate (22), and retain the structure (30) immovable relative to the substrate (22) in a sense direction (42). The compliant members (36) enable movement of the proof mass (28) in the sense direction (42). Movable fingers (38) extending from the proof mass (28) are disposed between fixed fingers (46) extending from the frame structure (30) to form a differential capacitive structure.

Abstract: The method and apparatus in one embodiment may have: providing a two-dimensional axisymmetric oscillator having a beam containing two principal elastic axes and two principal damping axes; driving the beam with drive components to oscillate across corners of the beam at approximately 45 degrees to sides of the beam, the drive components having forcer components that provide drive and pickoff components that provide feedback; and oscillating the beam in a normal mode and a reverse mode.

Abstract: The invention relates to a vibration measurement system for frequency-selective oscillation measurement in particular of low frequencies as are relevant in the field of automation and drive technology. The invention proposes coupling a broadband transmitter structure, which is excited directly by the excitation signal to be determined, via an electrostatic or inductive force to a receiver structure. This force coupling results in amplitude modulation of a carrier signal exciting the receiver structure. The actual excitation signal can be extracted from the spectrum of the amplitude-modulated carrier signal, for example by suitably selecting the frequency of the carrier signal. In order to make an oscillation analysis possible which is as unsusceptible to interference possible, an interference signal brought about, for example, by connector excitations is largely eliminated in advance from the amplitude-modulated carrier signal.

Abstract: A microstructure device is made by processing a material substrate consisting of e.g. a first process layer, a second process layer and a middle layer arranged between the first and the second process layers. The microstructure device includes a first structural part and a second structural part that has a portion facing the first structural part via a gap. The first and the second structural parts are connected to each other by a connecting part extending across the gap. This connecting part is formed in the first process layer to be in contact with the middle layer. The microstructure device also includes a protective part extending from the first structural part toward the second structural part or vice versa. The protective part is formed in the first or second process layer to be in contact with the middle layer.

Abstract: The present invention provides, in a physical quantity measuring system using a vibrator, a supporting structure of a vibrator for reducing the zero-point temperature drift of detection signal. It is provided a supporting member for supporting a vibrator with bonding wires. The supporting member has a supporting plate with an opening formed therein to be positioned direct under a vibrator, and a bonding wire comprising a bonding end to be bonded with the vibrator, a fixed portion fixed on the supporting plate and a bent portion direct under the opening. A distance “L1” between the bent portion and a position where the bonding wire starts to protrude from the supporting plate is 10 percent or more of a distance “L2” of the bent portion and the bonding end.

Abstract: To provide a compact and high performance gyroscope. A gyroscope (10) comprises an outer frame (11); an inner frame (12) positioned inside the outer frame and supported to be movable in one reciprocating direction; a plurality of proof masses (15) positioned inside the inner frame and supported to be movable in the direction orthogonal to the one reciprocating direction; a plurality of outer support suspensions (13) which connect the outer frame and the inner frame; a plurality of inner support suspensions (14) which connect the inner frame and each of the proof masses; actuators (16) for accelerating each of the proof masses; and detectors (17) for detecting displacement of the inner frame against the outer frame. The actuators oscillate the plurality of proof masses in-phase, and wherein Coriolis forces induced on each of the proof masses are summed up in the inner frame.

Abstract: An integrated MEMS structure includes a driving assembly anchored to a substrate and actuated with a driving movement. A pair of sensing masses suspended above the substrate and coupled to the driving assembly via elastic elements is fixed in the driving movement and performs a movement along a first direction of detection, in response to an external stress. A coupling assembly couples the pair of sensing masses mechanically to couple the vibration modes. The coupling assembly is formed by a rigid element, which connects the sensing masses and has a point of constraint in an intermediate position between the sensing masses, and elastic coupling elements for coupling the rigid element to the sensing masses to present a first stiffness to a movement in phase-opposition and a second stiffness, greater than the first, to a movement in phase, of the sensing masses along the direction of detection.

Abstract: A high-performance angular rate detecting device is provided. A driving part including a drive frame and a Coriolis frame is leviated by at least two fixing beams which share a fixed end and are extending in a direction orthogonal to a driving direction, thereby vibrating the driving part. Even when a substrate is deformed by mounting or heat fluctuation, internal stress generated to the fixed beam and a supporting beam is small, thereby maintaining a vibrating state such as resonance frequency and vibration amplitude constant. Therefore, a high-performance angular rate detecting device which is robust to changes in mounting environment can be obtained.

Abstract: The present invention relates to a novel silicon micromechanical gyroscope, which is used in control technology field to measure pose measurement of a rotating body, such as aerobat, motor tire and drilling platform, wherein the novel silicon micromechanical gyroscope main includes a sensing element and a signal process circuit. The sensing element further comprises a silicon slice frame, a silicon slice, an upper electrode ceramics plate and a bottom electrode ceramics plate. The signal process circuit further comprises a signal detecting bridge circuit used as bridge arm of the capacitor sensing element, and a SCM signal process circuit with data process module. The novel silicon micromechanical gyroscope is able to replace a drive force from the drive conformation with a rotating force from the rotation of the rotating body so as to achieve a novel silicon micromechanical gyroscope without a drive conformation.

Abstract: A high-performance angular rate detecting device is provided. A driving part including a drive frame and a Coriolis frame is levitated by at least two fixing beams which share a fixed end and are extending in a direction orthogonal to a driving direction, thereby vibrating the driving part. Even when a substrate is deformed by mounting or heat fluctuation, internal stress generated to the fixed beam and a supporting beam is small, thereby maintaining a vibrating state such as resonance frequency and vibration amplitude constant. Therefore, a high-performance angular rate detecting device which is robust to changes in mounting environment can be obtained.

Abstract: A sensor device includes a base plate, a seismic mass having an upper side and a lower side that is situated such that given acceleration of the base plate the seismic mass is capable of being displaced in a direction oriented non-parallel to the upper side and/or to the lower side, at least one raised stop on the seismic mass, and a detection and evaluation device that is adapted to acquire a displacement movement of the seismic mass relative to the base plate and, taking into account the displacement movement, to determine an item of information relating to an acceleration of the sensor device and/or to a force acting on the sensor device, the seismic mass having at least one resilient area that includes the at least one stop and at least one displaceable remaining area, and the resilient area being connected to the remaining area via at least one spring. A method is for manufacturing a sensor device.

Abstract: A micromechanical rotation rate sensor including at least one substrate, wherein the base surface of the substrate is oriented parallel to the x-y plane of a Cartesian coordinate system, at least two seismic masses and in each case at least one suspension spring element for suspending the seismic mass from the substrate, wherein the at least two seismic masses are coupled to one another by at least one coupling bar, and at least one of the suspension spring elements includes at least two bar sections, which, in the undeflected state, are oriented essentially parallel to one another or are at an angle of less than 45° with respect to one another, and one or more connecting sections, which connect the bar sections to one another, wherein the bar sections can be displaced relative to one another in their longitudinal direction.

Abstract: A dynamic quantity sensor includes a base, a sensor chip made of a rectangular board having a corner portion, and a bump. The sensor chip includes a detector, and a plurality of pads. The detector has a movable part, which is displaceable when a dynamic quantity is applied thereto, and detects the dynamic quantity based on a capacitance variation in accordance with a displacement of the movable part. The bump connects the plurality of pads of the sensor chip and the base. The corner portion of the sensor chip is released from the base such that the plurality of pads of the sensor chip is arranged at a location a predetermined distance from the corner portion of the sensor chip.

Abstract: The microsystem achieved in a flat substrate and comprises two oscillating masses connected to the substrate by suspension springs. The oscillating masses are coupled by a rigid coupling bar so as to produce an anti-phase movement of said oscillating masses when excitation of the latter is performed in a predefined excitation direction. The coupling bar is connected to intermediate zones of the corresponding suspension springs arranged on opposite sides of the oscillating masses. The intermediate zones are arranged between a first end of the suspension springs fixed to the corresponding oscillating mass, and a second end of the suspension springs fixed to the substrate by a corresponding anchoring point.

Abstract: An integrated microelectromechanical structure is provided with: a driving mass, anchored to a substrate via elastic anchorage elements and moved in a plane with a driving movement; and a first sensing mass, suspended inside, and coupled to, the driving mass via elastic supporting elements so as to be fixed with respect to the driving mass in the driving movement and to perform a detection movement of rotation out of the plane in response to a first angular velocity; the elastic anchorage elements and the elastic supporting elements cause the detection movement to be decoupled from the driving movement. The elastic supporting elements are coupled to the first sensing mass at an end portion thereof, and the axis of rotation of the detection movement extends, within the first sensing mass, only through the end portion.

Abstract: The invention relates to a microgyroscope, that is to say an inertial micromechanical sensor dedicated to the measurement of angular velocities, which is produced by micromachining techniques, and has a novel arrangement of the modules for measuring the movement of the vibrating masses. The gyroscope comprises two symmetrical moving assemblies (30, 50; 30?, 50?) that are coupled by a coupling structure (20, 20?, 22). Each of the two assemblies comprises a moving mass (30) surrounded by a moving intermediate frame (50). The frame (50) is connected to the coupling structure (20, 20?, 22) and can vibrate in two degrees of freedom in orthogonal directions Ox and Oy of the plane of the wafer. The mass (30) is connected, on one side, to the frame and, on the other side, to fixed anchoring regions (34, 36) via linking means (40-46; 52-58) that allow the vibration movement in the Oy direction to be transmitted to the mass without permitting any movement of the mass in the Ox direction.

Abstract: A microelectromechanical system (MEMS) includes a housing defining an enclosed cavity, stator tines extending from the housing into the cavity, a MEMS device located within the cavity, the MEMS device including a proof mass and rotor tines extending from the proof mass, each rotor tine being positioned at a capacitive distance from a corresponding stator tine. The rotor tines include a first section extending a first distance from an insulating layer of the rotor tines and a second section extending a second distance from the insulating layer in an opposite direction from the first section. The stator tines include a first section extending a first distance from an insulating layer of the stator tines and a second section extending a second distance from the insulating layer in an opposite direction from the first section, the stator tine first distance being greater than the rotor tine first distance.

Abstract: In an acceleration sensor, a first vibrator is arranged on a surface of a substrate such that the vibrator can vibrate in an X-axis direction. An angular-velocity-detecting vibrator is arranged inside the first vibrator such that the vibrator can be displaced in a Y-axis direction. A vibration generating unit and a vibration monitor unit are provided between the substrate and the first vibrator. An angular-velocity-detecting displacement detecting unit is provided between the substrate and the angular-velocity-detecting vibrator. A second vibrator is provided outside the first vibrator such that the vibrator can be displaced in the Y-axis direction. An acceleration-detecting displacement detecting unit is provided between the first and second vibrators. An angular velocity detecting circuit detects angular velocity by performing synchronous detection on a displacement detection signal from the displacement detecting unit using a monitor signal from the vibration monitor unit.

Abstract: A sensor that measures angular velocity about an axis that is normal to a sensing plane of the sensor. The sensor comprises a sensing subassembly that includes a planar frame parallel to the sensing plane, a first proof mass disposed in the sensing plane, a second proof mass disposed in the sensing plane laterally to the first proof mass, and a linkage within the frame and connected to the frame. The linkage is connected to the first proof mass and to the second proof mass. The sensor further includes actuator for driving the first proof mass and the second proof mass into oscillation along a drive axis in the sensing plane. The sensor further includes a first transducer to sense motion of the frame in response to a Coriolis force acting on the oscillating first proof mass and the oscillating second proof mass.

Abstract: For driving and simultaneously evaluating a deflection and/or a rate of motion of an electrostatically excited oscillator element, excitation currents flowing during electrostatic excitation are determined, and deflection and/or the rate of motion of the oscillator element are determined based on the determined excitation currents.

Abstract: Vibration gyro circuitry, a vibration gyro unit, and a method for detecting a vibration gyro output, which enable detection of a rotational angular velocity with high sensitivity, are provided. The circuitry and the unit includes a differential amplifier circuit (4) for outputting a signal Vda corresponding to a difference (Vgl?Vgr) between output signals of two detection pieces of a vibration gyro (31), a synchronous detection circuit (5) for synchronously detecting the output signal Vda of the differential amplifier circuit (4), and a phase shift circuit for supplying to the synchronous detection circuit (5) a signal, as a timing signal Vck for the synchronous detection, which is phase-shifted with respect to a drive signal (an output signal of an adding circuit 1) Vsa supplied to the vibration gyro (31).

Abstract: According to the present invention, an in-plane sensor comprises a structure unit which includes: a fixed structure including a fixed finger and a fixed column connected to each other, the fixed finger having a supported end supported by the fixed column and a suspended end; and a movable structure including at least one proof mass which surrounds the fixed finger in a horizontal plane.

Abstract: A micro-machined MEMS resonator gyroscope and accelerometer is fabricated from an epilayer semiconductor wafer to incorporate a substantially planar, H-shaped resonator mass suspended from a support plate by two opposed elongated springs that couple to the relatively short crossbar member of the H. The masses are harmonically oscillated relative to the support plate and a baseplate portion, and two orthogonal modes of the structure corresponding to the two nearly degenerate fundamental torsional modes thereof are used for sensing angular rate about one axis, and linear acceleration along two axes, of the sensor. The H-shaped mass advantageously incorporates a relatively high length-to-width aspect ratio, and in one embodiment, the springs may advantageously incorporate either a square cross-section, such that the structure can be tuned to substantially match the fundamental frequencies of the two resonance modes of the structure by removing, e.g.

Abstract: A resonant structure for a micromechanical device includes a crystalline silicon beam and at least one mass attached to the beam. An excitation plane of the resonant structure is defined by the predominant motion of the excited resonant structure. The beam includes crystal axes aligned such that none of the crystal axes are parallel to the length of the beam and/or none of the crystal axes are normal to the excitation plane.

Abstract: A physical quantity sensor includes: a substrate; a movable element; two fixed elements; a carrier wave application element for applying two carrier waves to the fixed elements; a signal application element for applying a middle voltage to the movable element; and a detection circuit for detecting a physical quantity. The detection circuit executes a first self diagnosis process when the signal application element further applies a first self diagnosis signal to the movable element. The first self diagnosis signal has a first frequency for obtaining a resonant magnification equal to or larger than 1.1 times with respect to a resonant frequency of the movable element, so that the movable element is resonated and almost contacts or press contacts one fixed element. The detection circuit determines whether a sticking phenomenon occurs when the signal application element applies the first self diagnosis signal.

Abstract: An angular velocity sensor includes a supporting substrate, a detecting portion, a displacement detecting portion, a first driving portion, and a second driving portion. The detecting portion is supported by the supporting substrate movably in at least a free direction. The displacement detecting portion detects a displacement of the detecting portion in the free direction. The first driving portion excites a first reference oscillation of at least a portion of the detecting portion so that a first Coriolis' force in the free direction is generated in response to an angular velocity about a first axis. The second driving portion excites a second reference oscillation of at least a portion of the detecting portion so that a second Coriolis' force in the free direction is generated in response to an angular velocity about a second axis.

Abstract: Disclosed is an acceleration sensor having a small variation in detection sensitivity, in which one end portion of an oscillation detecting element is fixed so that the free length thereof does not vary. Supporting resins 4a, 4b are formed in one end portion of the oscillation detecting element 3. With the oscillation detecting element being inserted into a through hole 2h of a holding member 2 provided in a case 1, the supporting resins 4a, 4b are in close contact with the inner periphery of the through hole 2h. As a result, the oscillation detecting element 3 is fixed to and held by the holding member 2.

Abstract: An angular rate sensor includes: a substrate; a drive-purpose vibrator capable of vibrating in a first direction; and an angular velocity detection-purpose vibrator capable of vibrating in a second direction. The sensor detects an angular velocity on the basis of vibration of the angular velocity detection-purpose vibrator in the second direction caused by a Coriolis force, when the drive-purpose vibrator is vibrated in the first direction, and the angular velocity is applied to the sensor in a third direction. The angular velocity detection-purpose vibrator has a length along with the second direction and a width along with the first direction. A ratio between the width and the length is equal to or larger than 0.1.

Abstract: An angular rate sensor for detecting a rotation includes a substrate, at least one oscillating element that can be excited so as to oscillate rotationally or radially, an anchor structure, one or several detecting elements, one or several joining elements that connect the detecting element/s to the oscillating element, a mechanism for exciting the oscillating element, and a device for detecting a radial or rotational oscillation of the detecting element/s. Each of the detecting elements can oscillate radially on the same plane on which rotational oscillation of the oscillating element occurs, or vice versa, while the centrifugal force Fz caused by the rotational oscillation will not cause any significant radial movement of the detecting element/s or the oscillating elements. Also disclosed are different methods for operating said sensor.

Abstract: In an acceleration sensor, a first vibrator is arranged on a surface of a substrate such that the vibrator can vibrate in an X-axis direction. An angular-velocity-detecting vibrator is arranged inside the first vibrator such that the vibrator can be displaced in a Y-axis direction. A vibration generating unit and a vibration monitor unit are provided between the substrate and the first vibrator. An angular-velocity-detecting displacement detecting unit is provided between the substrate and the angular-velocity-detecting vibrator. A second vibrator is provided outside the first vibrator such that the vibrator can be displaced in the Y-axis direction. An acceleration-detecting displacement detecting unit is provided between the first and second vibrators. An angular velocity detecting circuit detects angular velocity by performing synchronous detection on a displacement detection signal from the displacement detecting unit using a monitor signal from the vibration monitor unit.

Abstract: A high-performance angular rate detecting device is provided. A driving part including a drive frame and a Coriolis frame is levitated by at least two fixing beams which share a fixed end and are extending in a direction orthogonal to a driving direction, thereby vibrating the driving part. Even when a substrate is deformed by mounting or heat fluctuation, internal stress generated to the fixed beam and a supporting beam is small, thereby maintaining a vibrating state such as resonance frequency and vibration amplitude constant. Therefore, a high-performance angular rate detecting device which is robust to changes in mounting environment can be obtained.

Abstract: A drive arrangement for a micromachine includes a plurality of fixed electrodes arranged so as to have a common centroid.

Abstract: Angular rate sensor for detecting rotation about first and second mutually perpendicular axes which has first and second masses coupled together for torsional drive mode oscillation of equal amplitude and opposite phase about third axes which are perpendicular to the first and second axes. The first mass is mounted for oscillation about the second axis in response to Coriolis forces produced by rotation about the first axis, and the second mass is mounted for oscillation about the first axis in response to Coriolis forces produced by rotation about the second axis. In some disclosed embodiments, the rate sensor also includes a pair of accelerometer masses which are connected together for torsional movement of equal amplitude and opposite phase about axes parallel to the third axes in response to acceleration along the second axis and for torsional movement of equal amplitude and opposite phase about axes parallel to the second axis in response to acceleration along the third axes.

Abstract: Vibration gyro circuitry, a vibration gyro unit, and a method for detecting a vibration gyro output, which enable detection of a rotational angular velocity with high sensitivity, are provided. The circuitry and the unit includes a differential amplifier circuit (4) for outputting a signal Vda corresponding to a difference (Vgl?Vgr) between output signals of two detection pieces of a vibration gyro (31), a synchronous detection circuit (5) for synchronously detecting the output signal Vda of the differential amplifier circuit (4), and a phase shift circuit for supplying to the synchronous detection circuit (5) a signal, as a timing signal Vck for the synchronous detection, which is phase-shifted with respect to a drive signal (an output signal of an adding circuit 1) Vsa supplied to the vibration gyro (31).

Abstract: MEMS devices and methods for measuring Coriolis forces using force rebalancing and parametric gain amplification techniques are disclosed. A MEMS inertial sensor can include one or more proof masses, at least one sense electrode positioned adjacent to each proof mass, a number of torquer electrodes for electrostatically nulling quadrature and Coriolis-related proof mass motion, and a number of pump electrodes for producing a pumping force on the proof masses. Force rebalancing voltages can be applied to some torquer electrodes to electrostatically null quadrature and/or Coriolis-related proof mass motion along a sense axis of the device. A pumping voltage at approximately twice the motor drive frequency of the proof masses can be used to pump the proof masses along the sense axis.

Abstract: MEMS devices and methods employing one or more electrodes coupled to a time-varying rebalancing voltage are disclosed. A MEMS inertial sensor in accordance with an illustrative embodiment can include one or more proof masses, at least one sense electrode positioned adjacent to each proof mass, and one or more torquer electrodes. Rebalancing voltages can be applied to the torquer electrodes to electrostatically null quadrature and/or Coriolis-related proof mass motion along a sense axis of the device. The rebalancing voltages applied to each of the torquer electrodes can be adjusted using feedback from one or more force rebalancing control loops.

Abstract: MEMS devices and methods for measuring Coriolis forces using force rebalancing and parametric gain amplification techniques are disclosed. A MEMS inertial sensor can include one or more proof masses, at least one sense electrode positioned adjacent to each proof mass, a number of torquer electrodes for electrostatically nulling quadrature and Coriolis-related proof mass motion, and a number of pump electrodes for producing a pumping force on the proof masses. Force rebalancing voltages can be applied to some torquer electrodes to electrostatically null quadrature and/or Coriolis-related proof mass motion along a sense axis of the device. A pumping voltage at approximately twice the motor drive frequency of the proof masses can be used to pump the proof masses along the sense axis.

Abstract: An inertial sensor includes a cross-quad configuration of four interconnected sensor elements. Each sensor element has a frame and a resonator suspended within the frame. The sensor elements are arranged so that the frames of adjacent sensor elements are allowed to move in anti-phase to one another but are substantially prevented from moving in phase with one another. The sensor elements may be configured in a horizontally coupled arrangement, a vertically coupled arrangement, or a fully coupled arrangement. A pair of sensor elements may be vertically coupled.

Abstract: A gimbal-type torsional z-axis micromachined gyroscope with a non-resonant actuation scheme measures angular rate of an object with respect to the axis normal to the substrate plane (the z-axis). A 2 degrees-of-freedom (2-DOF) drive-mode oscillator is comprised of a sensing plate suspended inside two gimbals. By utilizing dynamic amplification of torsional oscillations in the drive-mode instead of resonance, large oscillation amplitudes of the sensing element is achieved with small actuation amplitudes, providing improved linearity and stability despite parallel-plate actuation. The device operates at resonance in the sense direction for improved sensitivity, while the drive direction amplitude is inherently constant within the same frequency band.

Abstract: The present invention discloses an inertial sensor comprising a planar mechanical resonator with embedded sensing and actuation for substantially in-plane vibration and having a central rigid support for the resonator. At least one excitation or torquer electrode is disposed within an interior of the resonator to excite in-plane vibration of the resonator and at least one sensing or pickoff electrode is disposed within the interior of the resonator for sensing the motion of the excited resonator. In one embodiment, the planar resonator includes a plurality of slots in an annular pattern; in another embodiment, the planar mechanical resonator comprises four masses; each embodiment having a simple degenerate pair of in-plane vibration modes.

Abstract: The apparatus in one embodiment may have: a beam having at least first and second mounting points that are operatively coupled to the beam by first and second flexures, respectivly; the beam having first and second nodal points; the beam having a center area; and an altered mass content in a vicinity of the center area, the altered mass content being such that the first and second nodal points are substantially aligned with the first and second flexures. The beam is therefore supported at the nodal points for the fundamental mode of vibration.

Abstract: A method for manufacturing a quartz oscillator having a stable temperature drift characteristic attributed to the quartz oscillating piece and a quartz oscillator are disclosed. The method comprises a quartz crystal etching step S1 of processing a quartz oscillating piece into a predetermined shape by etching, an electrode membrane forming step S2 of forming an electrode on the quartz oscillating piece, a quartz crystal mounting step S3 of mounting the quartz oscillating piece in an oscillator package, a leakage oscillation adjusting step S4 of driving the mounted quartz oscillating piece, detecting the leakage oscillation, and removing a part of the quartz oscillating piece depending on the detected leakage oscillation, and a re-etching step S6 of re-etching the quartz oscillating piece subjected to the removal.

Abstract: This invention suggests a micro-gyrometer, advantageously machined using conventional micro-electronic techniques, based on the detection of Coriolis forces generated by an angular movement ? perpendicular to the direction of vibration of the masses free to move along the plane of the gyrometer. Coriolis forces are detected through the movement that they apply to the natural mode of a resonator coupled to the moving device.

Abstract: A micro-electromechanical (MEM) device includes a proof mass resiliently mounted to a substrate. The proof mass has first and second combs formed on opposite sides thereof and is electrically coupled to ground. A fixed drive comb is interleaved with the first comb of the proof mass. A fixed pick-off comb is interleaved with a portion of the second comb of the proof mass. A fixed bias comb is interleaved with the second proof mass comb. A substantially direct current (DC) bias is applied to the fixed bias comb. A substantially constant voltage is also exerted on a sense plate beneath the proof mass. The sense plate and bias comb are coupled to a charge amp through capacitors such that transient currents induced by motion of the proof mass will cause current to flow to a charge amp.

Abstract: A four-degrees-of-freedom (DOF) nonresonant micromachined gyroscope utilizes a dynamical amplification both in the drive-direction oscillator and the sense-direction oscillator, which are structurally decoupled, to achieve large oscillation amplitudes without resonance. The overall dynamical system is comprised of three proof masses. The second and third masses form the sense-direction oscillator. The first mass and the combination of the second and third masses form the drive-direction oscillator. The frequency responses of the drive and sense-mode oscillators have two resonant peaks and a flat region between the peaks. The device is nominally operated in the flat regions of the response curves belonging to the drive and sense-mode oscillators, where the gain is less sensitive to frequency fluctuations. This is achieved by designing the drive and sense anti-resonance frequencies to match.

Abstract: A mass includes a first set of drive fingers interdigitated with a first array of fixed drive fingers and a second set of drive fingers interdigitated with a second array of fixed drive fingers. Each array of fixed drive fingers is affixed to a substrate using a plurality of anchors. The anchors for the first and second arrays of fixed drive fingers are arranged to be co-linear in a lateral direction relative to the motion of the mass.

Abstract: A closed-loop, comb drive device that reduces certain “common mode” sensor errors. The device includes a comb structure, electronics, a substrate, and a position sensor. The comb structure includes two comb-drive sections, each having at least two subsections. The comb drive sub-sections in each section are positioned in a diagonal relationship to each other relative to the device axes. A separate pick-off section, along with the electronics, determine which of the two drive sections should receive a voltage differential, and the size of that differential. The diagonal relationship within each drive section eliminates many of the large scale factor errors which often occur in prior-art designs.

Abstract: A coupling apparatus allows anti-phase movements of inertial sensor element frames along parallel axes but substantially prevents in-phase movements of the frames. The coupling apparatus includes a bar coupled between first and second sensor element frames and at least one supporting structure supporting the bar. The at least one structure is coupled to a substrate underlying the frames. The structures allow the bar to rotate at a pivot point when the frames move in anti-phase to one another along substantially parallel axes but substantially prevent in-phase movements of the frames.

Abstract: A Coriolis gyro includes a first and a second resonator, each in the form of a coupled system comprising first and second linear oscillators. The first resonator can be caused to oscillate in antiphase with respect to the second resonator along a common oscillation axis. A system coupled in this way has the advantage that it is possible to measure rotation rate and acceleration simultaneously, with insensitivity to disturbances (e.g., externally or internally acting vibrations).