A MEMS type inertial sensor comprising a support structure having at least a first seismic body and a second seismic body connected thereto by resilient means in order to be movable in a suspension plane, transducers for maintaining the seismic bodies in vibration and for determining movements of the seismic bodies in the suspension plane, and a control unit connected to the transducers by electrical conductor means. The transducers comprise at least one electrode secured to the first seismic body and at least one electrode secured to the second seismic body, the two electrodes being arranged to enable relative movements of the seismic bodies relative to each other in the suspension plane to be measured directly.

For a small sensor produced through a MEMS process, when an electrode pad, wiring, or a shield layer is formed in a final step, it is difficult to nondestructively investigate whether a structure for sensing a physical quantity has been processed satisfactorily. In the present invention, in a physical quantity sensor formed from an MEMS structure, in a structure in which a surface electrode having through wiring is formed on the surface of an electrode substrate and the periphery thereof is insulated, forming a shield layer comprising a metallic material on the surface of the electrode substrate in a planar view and providing a space for internal observation inside the shield layer makes it possible to check for internal defects.

For a small sensor produced through a MEMS process, when an electrode pad, wiring, or a shield layer is formed in a final step, it is difficult to nondestructively investigate whether a structure for sensing a physical quantity has been processed satisfactorily. In the present invention, in a physical quantity sensor formed from an MEMS structure, in a structure in which a surface electrode having through wiring is formed on the surface of an electrode substrate and the periphery thereof is insulated, forming a shield layer comprising a metallic material on the surface of the electrode substrate in a planar view and providing a space for internal observation inside the shield layer makes it possible to check for internal defects.

.[.The.]. .Iadd.An .Iaddend.angular velocity sensor .[.of the present invention.]. has one end connected to .Iadd.a .Iaddend.holding section and .[.the other.]. .Iadd.another .Iaddend.end connected to .Iadd.a .Iaddend.weighting section. According to the angular velocity sensor, .Iadd.a .Iaddend.driving arm has a .[.dog-leg.]. .Iadd.bent .Iaddend.structure of arms extending in a direction perpendicular to a connecting direction of .Iadd.the .Iaddend.holding section and .Iadd.the .Iaddend.weighting section.

.[.The.]. .Iadd.An .Iaddend.angular velocity sensor .[.of the present invention.]. has one end connected to .Iadd.a .Iaddend.holding section and .[.the other.]. .Iadd.another .Iaddend.end connected to .Iadd.a .Iaddend.weighting section. According to the angular velocity sensor, .Iadd.a .Iaddend.driving arm has a .[.dog-leg.]. .Iadd.bent .Iaddend.structure of arms extending in a direction perpendicular to a connecting direction of .Iadd.the .Iaddend.holding section and .Iadd.the .Iaddend.weighting section.

A vibrating body of an angular velocity detection element includes detection beams extending in a cross shape from a central base and external connection beams and internal connection beams connected between adjacent detection beams. The detection beams each include a base end detection beam that is connected to the central base and a central detection beam, a left detection beam and a right detection beam that define three prongs. The central detection beam is connected to the external connection beams on both sides, the left detection beam is connected to the internal connection beam on the left side and the right detection beam is connected to the internal connection beam on the right side. The adjacent external connection beams undergo driven vibration so as to be displaced in directions so as to have mirror relationships with each other with the detection beams interposed between the external connection beams acting as boundaries therebetween.

A vibrating body of an angular velocity detection element includes detection beams extending in a cross shape from a central base and external connection beams and internal connection beams connected between adjacent detection beams. The detection beams each include a base end detection beam that is connected to the central base and a central detection beam, a left detection beam and a right detection beam that define three prongs. The central detection beam is connected to the external connection beams on both sides, the left detection beam is connected to the internal connection beam on the left side and the right detection beam is connected to the internal connection beam on the right side. The adjacent external connection beams undergo driven vibration so as to be displaced in directions so as to have mirror relationships with each other with the detection beams interposed between the external connection beams acting as boundaries therebetween.

Various embodiments of the invention integrate multiple shock-robust single-axis MEMS gyroscopes into a single silicon substrate while avoiding the complexities typically associated with designing a multi-drive control system for shock immune gyroscopes. In certain embodiments of the invention, a shock immune tri-axial MEMS gyroscope is based on a driving scheme that employs rotary joints to distribute driving forces generated by two sets of driving masses to individual sensors, thereby, simplifying the control of the gyroscope.

Various embodiments of the invention integrate multiple shock-robust single-axis MEMS gyroscopes into a single silicon substrate while avoiding the complexities typically associated with designing a multi-drive control system for shock immune gyroscopes. In certain embodiments of the invention, a shock immune tri-axial MEMS gyroscope is based on a driving scheme that employs rotary joints to distribute driving forces generated by two sets of driving masses to individual sensors, thereby, simplifying the control of the gyroscope.

A sensor is disclosed for detecting a rotational motion about a resulting sensitivity axis. The sensor includes at least two dual mass gyroscope units, each of the gyroscope units are adapted to detect a rotational motion about a sensitivity axis of the respective gyroscope unit. The sensitivity axes being parallel to each other and to the resulting sensitivity axis. The gyroscope units are interconnected at the inertial masses of the gyroscope units which cause the gyroscope unit to operate synchronously.