Abstract: A sensing device comprises a rotationally oscillating proof mass resonator and a detector resonator. The detector resonator, actuated to produce an oscillating signal, is coupled to the proof mass resonator and the frequency of the oscillating signal is modulated by a change of motion of the proof mass resonator.

Abstract: A sensing device comprises a rotationally oscillating proof mass resonator and a detector resonator. The detector resonator, actuated to produce an oscillating signal, is coupled to the proof mass resonator and the frequency of the oscillating signal is modulated by a change of motion of the proof mass resonator.

Abstract: A micro gyro consisting of a vibrating micro scale structure produces a signal whose characteristic frequency shifts in proportion to the applied angular velocity. The vibrating structure consists of a suspended proof mass resonator supported on springs and connected to at least one detector resonator. The structure can be made with multiple semiconductor materials such as silicon, poly-silicon, silicon dioxide, and silicon nitride, using one of many MEMS fabrication processes. The proof mass resonator is designed to have two closely coupled resonant frequencies, with one resonant mode for the drive motion and the second resonant mode for the sense motion. Detector resonators are connected to the vibrating structure such that when the proof mass resonator oscillates due to the Coriolis force in its sense mode, the connections to the detector resonators are stressed by the proof mass resonator, thus changing the resonant frequency of the detector resonators.

Abstract: A micro gyro consisting of a vibrating micro scale structure produces a signal whose characteristic frequency shifts in proportion to the applied angular velocity. The vibrating structure consists of a suspended proof mass resonator supported on springs and connected to at least one detector resonator. The structure can be made with multiple semiconductor materials such as silicon, poly-silicon, silicon dioxide, and silicon nitride, using one of many MEMS fabrication processes. The proof mass resonator is designed to have two closely coupled resonant frequencies, with one resonant mode for the drive motion and the second resonant mode for the sense motion. Detector resonators are connected to the vibrating structure such that when the proof mass resonator oscillates due to the Coriolis force in its sense mode, the connections to the detector resonators are stressed by the proof mass resonator, thus changing the resonant frequency of the detector resonators.

Abstract: Disclosed is a micro-gyro and method of driving a micro-gyro. The method and structure are embodied in a micro-gyro of the type where first flexures extend from an anchor connect to a sense plate, where second flexures extend from the sense plate connect to a drive ring, where the drive ring is driven to oscillate about a drive axis, and where the first flexures constrain the sense plate from moving about the drive axis but permit the sense plate and the attached drive ring to rock about a sense axis. The sense plate, drive ring and flexures form a plate-ring-flexure system that is tuned such that the system rocks about the sense axis in a first or fundamental mode where the plate and ring move substantially in phase at the lowest resonant frequency.

Abstract: Rotation of an inertial mass included in the gyro is produced by applying a torque to the inertial mass about a rate axis orthogonal to the drive axis along or about which the drive motion of the inertial mass is defined. The torque is applied by created a potential difference between interdigitated finger electrodes, by a piezoelectric element or any other known or later discovered means. The combination of the drive motion and the torque produces a Coriolis force which produces a displacement of a sense element coupled to the inertial mass or a displacement of the inertial mass itself. The induced rotation about the rate axis simulates the angular momentum which would be produced in the gyro by a precision rate table. This displacement or response is then an empirical parameter which characterizes the gyro's response to a simulated rate table test and can then be used to generate a correction factor for the gyro and to thus calibrate it.

Abstract: Disclosed is a method of correcting quadrature error in a dynamically decoupled micro-gyro (100, 200) having a drive mass (110, 210) that is vibrated relative to a drive axis (Y, Z) and a sense mass (111, 211) that responds to the drive mass (110, 210) in the presence of an angular rate and associated coriolis force by vibrating relative to a sense axis (X, Y). The method includes the steps of providing a first static force element (121, 221) for applying a first steady-state force to a first region of the drive mass (110, 210); providing a second static force element (122, 222) for applying a second steady-state force to a second region of the drive mass (210), and applying a corrective steady-state force to the drive mass (110, 210) with the first and second static force elements (121, 122; 221, 222), the corrective steady-state force making the drive axis (Y, Z) of the drive mass (110, 210) orthogonal to the sense axis (X, Y) of the sense mass (111, 211).

Abstract: Disclosed is a microelectromechanical sensor (10) with an element (40) that is driven into oscillations with drive forms (&phgr;1, &phgr;2, &phgr;3, &phgr;4) through the use of arms (50), comb-drives (55A, 55B, 55C, and 55D) and corresponding comb-fingers (51, 61) and wherein a sense signal is transduced with capacitive sense electrodes (26, 26). The driveforms (&phgr;1, &phgr;2, &phgr;3, &phgr;4) are provided in four-phases and are applied in pairs (&phgr;1, &phgr;3 and &phgr;2, &phgr;4) that are 180 degrees out of phase with respect to one another such that the driveforms are substantially self-canceling with regard to any driveform energy that feeds through any parasitic capacitance (99) that connects the comb-drives (55A, 55B, 55C, and 55D) to the capacitive sense electrodes (26, 26).

Abstract: Disclosed is a method of correcting quadrature error in a dynamically decoupled micro-gyro (100, 200) having a drive mass (110, 210) that is vibrated relative to a drive axis (Y, Z) and a sense mass (111, 211) that responds to the drive mass (110, 210) in the presence of an angular rate and associated coriolis force by vibrating relative to a sense axis (X, Y). The method includes the steps of providing a first static force element (121, 221) for applying a first steady-state force to a first region of the drive mass (110, 210); providing a second static force element (122, 222) for applying a second steady-state force to a second region of the drive mass (210), and applying a corrective steady-state force to the drive mass (110, 210) with the first and second static force elements (121, 122; 221, 222), the corrective steady-state force making the drive axis (Y, Z) of the drive mass (110, 210) orthogonal to the sense axis (X, Y) of the sense mass (111, 211).

Abstract: A micro-gyro device is disclosed combining a first element which oscillates linearly in a plane along a first direction, ad a second element which receives Coriolis force acting in the same plane along a second direction perpendicular to the first direction, so arranged that said Coriolis force is transmitted from one element to the other without any substantial transfer of motion of either element to the other in its own direction of motion. In other words, the masses of the two elements operate independently of one another, providing improved performance, and individual adjustability to compensate for any manufacturing imprecision. The rate axis, around which is measured angular speed of the micro-gyro device due to exterior forces, is perpendicular to the plane of the first and second elements.

Abstract: A micro-gyro device is disclosed combining an element which oscillates around the drive axis and an element which rocks around the output axis, so arranged that Coriolis force is transmitted from one element of the other without any substantial transfer of motion of either element to the other in its own direction of motion. In other words, the masses of the two elements operate independently of one another, providing improved performance, and individual adjustability to compensate for any manufacturing imprecision. The presently-preferred device combines an outer ring which oscillates around the drive axis with an inner disk which rocks around the output axis, whenever external rotating motion occurs about the rate axis.