Abstract: A rotation rate sensor including a substrate having a principal plane of extension, and a structure movable with respect to the substrate; the structure being excitable from a neutral position into an oscillation having a movement component substantially parallel to a driving direction, which is substantially parallel to the principal plane of extension. To induce the oscillation, the rotation rate sensor includes a comb electrode moved along with the structure and a comb electrode fixed in position relative to the substrate. The excitation is produced by applying a voltage to the moving comb electrode and/or to the stationary comb electrode. Due to a rotation rate of the rotation rate sensor about an axis running substantially perpendicularly to the driving direction and substantially perpendicularly to the detection direction, a force applied to the structure with a force component along a detection direction substantially perpendicular to the driving direction is detectable.

Abstract: A rotation rate sensor having a first structure movable with respect to the substrate, a second structure movable with respect to the substrate and with respect to the first structure, a first drive structure for deflecting the first structure with a motion component parallel to a first axis, and a second drive structure for deflecting the second structure with a motion component parallel to the first axis. The first and second structures are excitable to oscillate in counter-phase, with motion components parallel to the first axis, the first drive structure having a first spring mounted on the substrate to counteract a pivoting of the first structure around an axis parallel to a second axis extending perpendicularly to a principal extension plane, the second drive structure having a second spring mounted on the substrate to counteracts a pivoting of the second structure around a further axis parallel to the second axis.

Abstract: A rotation rate sensor includes first, second, third and fourth structures that are each movable relative to a substrate, a drive device configured to deflect each of the first, second, third, and fourth structures essentially parallel to a drive direction and out of respective resting positions of the first, second, third, and fourth structures, such that, at a first frequency, the first and fourth structures are excitable to an oscillation that is essentially in-phase relative to each other and essentially in phase-opposition relative to the second and third structures, and, at a second frequency, the first and second structures are excitable to an oscillation that is essentially in-phase relative to each other and essentially in phase-opposition relative to the third and fourth structures.

Abstract: A rotation rate sensor for detecting a rotational movement of the rotation rate sensor about a rotational axis extending within a drive plane of the rotation rate sensor include: a first rotational element, a second rotational element and a drive structure moveable in parallel to the drive plane, the first rotational element being drivable about a first center of rotation to achieve a first rotational vibration in parallel to the drive plane, the second rotational element being drivable about a second center of rotation to achieve a second rotational vibration in parallel to the drive plane, the drive structure being (i) coupled to the first and second rotational elements, and (ii) configured to generate a drive mode in phase opposition of the first and second rotational vibrations.

Abstract: A yaw rate sensor (10) includes a movable mass structure (12) and a drive component (13) which is suitable for setting the movable mass structure (12) in motion (14), and an analysis component (15) which is suitable for detecting a response (40) of the movable mass structure (12) to a yaw rate (?). A method for functional testing of a yaw rate sensor (10) includes the following steps: driving a movable mass structure (12), feeding a test signal (42) into a quadrature control loop (44) at a feed point (48) of the quadrature control loop (44), feeding back a deflection (40) of the movable mass structure (12), detecting a measure of the feedback of the movable mass structure (12), and reading out the response signal (47) from the quadrature control loop (44).

Abstract: A rotation-rate sensor having a substrate with main extension plane, for detecting a rotation rate, extending in a direction parallel/orthogonal to the main plane; the sensor including a primary/secondary pair of seismic masses; the primary pair having first/second primary masses; the secondary pair having first/second secondary masses; the first/second primary masses being movable relative to the substrate along a primary deflection direction extending parallel to the main plane; the first/second secondary masses being movable relative to the substrate along a secondary deflection direction extending parallel to the main plane; the first/second primary masses and the first/second primary masses being movable antiparallel or parallel to one another corresponding to the deflection direction, essentially extending orthogonally to the secondary deflection direction; and the primary pair and/or secondary pair being drivable so that, based on sensor rotation, the Coriolis force leads to deflection of the first/sec

Abstract: A yaw-rate sensor having a substrate and a plurality of movable substructures that are mounted over a surface of the substrate, the movable substructures being coupled to a shared, in particular, central spring element, means being provided for exciting the movable substructures into a coupled oscillation in a plane that extends parallel to the surface of the substrate, the movable substructures having Coriolis elements, means being provided for detecting deflections of the Coriolis elements induced by a Coriolis force, a first Coriolis element being provided for detecting a yaw rate about a first axis, a second Coriolis element being provided for detecting a yaw rate about a second axis, the second axis being oriented perpendicularly to the first axis.

Abstract: A yaw-rate sensor, having a substrate which has a main extension plane, for detecting a yaw rate about a first direction extending either parallel to the main extension plane or perpendicular to the main extension plane. The yaw-rate sensor has a drive device, a first Coriolis mass and a second Coriolis mass, the drive device being configured to drive at least one part of the first Coriolis mass and at least one part of the second Coriolis mass in a direction parallel to a drive direction extending perpendicular to the first direction.

Abstract: A yaw-rate sensor having a substrate and a plurality of movable substructures that are mounted over a surface of the substrate, the movable substructures being coupled to a shared, in particular, central spring element, means being provided for exciting the movable substructures into a coupled oscillation in a plane that extends parallel to the surface of the substrate, the movable substructures having Coriolis elements, means being provided for detecting deflections of the Coriolis elements induced by a Coriolis force, a first Coriolis element being provided for detecting a yaw rate about a first axis, a second Coriolis element being provided for detecting a yaw rate about a second axis, the second axis being oriented perpendicularly to the first axis.

Abstract: A yaw-rate sensor having a substrate and a plurality of movable substructures that are mounted over a surface of the substrate, the movable substructures being coupled to a shared, in particular, central spring element, means being provided for exciting the movable substructures into a coupled oscillation in a plane that extends parallel to the surface of the substrate, the movable substructures having Coriolis elements, means being provided for detecting deflections of the Coriolis elements induced by a Coriolis force, a first Coriolis element being provided for detecting a yaw rate about a first axis, a second Coriolis element being provided for detecting a yaw rate about a second axis, the second axis being oriented perpendicularly to the first axis.

Abstract: A yaw-rate sensor having a substrate and a plurality of movable substructures that are mounted over a surface of the substrate, the movable substructures being coupled to a shared, in particular, central spring element, means being provided for exciting the movable substructures into a coupled oscillation in a plane that extends parallel to the surface of the substrate, the movable substructures having Coriolis elements, means being provided for detecting deflections of the Coriolis elements induced by a Coriolis force, a first Coriolis element being provided for detecting a yaw rate about a first axis, a second Coriolis element being provided for detecting a yaw rate about a second axis, the second axis being oriented perpendicularly to the first axis.

Abstract: A rotation rate sensor for detecting a rotational movement of the rotation rate sensor about a rotational axis extending within a drive plane of the rotation rate sensor include: a first rotational element, a second rotational element and a drive structure moveable in parallel to the drive plane, the first rotational element being drivable about a first center of rotation to achieve a first rotational vibration in parallel to the drive plane, the second rotational element being drivable about a second center of rotation to achieve a second rotational vibration in parallel to the drive plane, the drive structure being (i) coupled to the first and second rotational elements, and (ii) configured to generate a drive mode in phase opposition of the first and second rotational vibrations.

Abstract: A rotation-rate sensor having a substrate with main extension plane, for detecting a rotation rate, extending in a direction parallel/orthogonal to the main plane; the sensor including a primary/secondary pair of seismic masses; the primary pair having first/second primary masses; the secondary pair having first/second secondary masses; the first/second primary masses being movable relative to the substrate along a primary deflection direction extending parallel to the main plane; the first/second secondary masses being movable relative to the substrate along a secondary deflection direction extending parallel to the main plane; the first/second primary masses and the first/second primary masses being movable antiparallel or parallel to one another corresponding to the deflection direction, essentially extending orthogonally to the secondary deflection direction; and the primary pair and/or secondary pair being drivable so that, based on sensor rotation, the Coriolis force leads to deflection of the first/sec

Abstract: A yaw rate sensor, including a substrate and a main extension plane, for detecting a yaw rate around a first direction in parallel to the main extension plane, a first Coriolis mass, and a second Coriolis mass, and a drive device configured to drive the first and second Coriolis masses in parallel to a drive direction perpendicular to the first direction, the first and second Coriolis masses, for a yaw rate around the first direction, experiencing a Coriolis acceleration in parallel to a detection direction, which is perpendicular to the drive and first directions, the first and second Coriolis masses having first/second partial areas and third/fourth partial areas, respectively. The first and third partial areas are farther from the axis of symmetry in parallel to the first direction, and the second and fourth partial areas are closer to the axis of symmetry in parallel to the first direction.

Abstract: A yaw-rate sensor having a substrate and a plurality of movable substructures that are mounted over a surface of the substrate, the movable substructures being coupled to a shared, in particular, central spring element, means being provided for exciting the movable substructures into a coupled oscillation in a plane that extends parallel to the surface of the substrate, the movable substructures having Coriolis elements, means being provided for detecting deflections of the Coriolis elements induced by a Coriolis force, a first Coriolis element being provided for detecting a yaw rate about a first axis, a second Coriolis element being provided for detecting a yaw rate about a second axis, the second axis being oriented perpendicularly to the first axis.

Abstract: A rotation rate sensor having a substrate including a main extension plane, force transmission elements that are movably fastened on the substrate using detection springs and a seismic mass are provided, the seismic mass being suspended over the force transmission elements, movably relative to the substrate, in such a way that the seismic mass is able to be excited, using a drive unit, to a drive vibration about a drive axis that is parallel to the main extension plane, and in response to the presence of a rotation rate that extends in parallel to the main extension plane and perpendicular to the drive axis, the seismic mass is excitable, as a result of Coriolis forces, to a detection vibration about a detection axis that is perpendicular to the main extension plane, the detection springs being connected to the force transmission elements in the region of the vibrational nodes.

Abstract: A yaw-rate sensor having a substrate and a plurality of movable substructures that are mounted over a surface of the substrate, the movable substructures being coupled to a shared, in particular, central spring element, where the movable substructures are excitable into a coupled oscillation in a plane that extends parallel to the surface of the substrate, the movable substructures having Coriolis elements, where deflections of the Coriolis elements induced by a Coriolis force are detectable, a first Coriolis element being provided for detecting a yaw rate about a first axis, a second Coriolis element being provided for detecting a yaw rate about a second axis, the second axis being oriented perpendicularly to the first axis.

Abstract: A yaw rate sensor (10) includes a movable mass structure (12) and a drive component (13) which is suitable for setting the movable mass structure (12) in motion (14), and an analysis component (15) which is suitable for detecting a response (40) of the movable mass structure (12) to a yaw rate (?). A method for functional testing of a yaw rate sensor (10) includes the following steps: driving a movable mass structure (12), feeding a test signal (42) into a quadrature control loop (44) at a feed point (48) of the quadrature control loop (44), feeding back a deflection (40) of the movable mass structure (12), detecting a measure of the feedback of the movable mass structure (12), and reading out the response signal (47) from the quadrature control loop (44).

Abstract: A yaw rate sensor is described which includes a drive device, at least one Coriolis element, and a detection device having at least two detection elements which are coupled to one another with the aid of a coupling device, the drive device being connected to the Coriolis element for driving a vibration of the Coriolis element, and an additional coupling device which is connected to the detection device and to the Coriolis element for coupling a deflection in the plane of vibration of the Coriolis element to the detection device in a direction orthogonal to the vibration.

Abstract: A yaw-rate sensor and a method for operating a yaw-rate sensor having a first Coriolis element and a second Coriolis element are proposed, the yaw-rate sensor having a substrate having a main plane of extension, the yaw-rate sensor having a first drive element for driving the first Coriolis element in parallel to a second axis, the yaw-rate sensor having a second drive element for driving the second Coriolis element in parallel to the second axis, the yaw-rate sensor having detection means for detecting deflections of the first Coriolis element and of the second Coriolis element in parallel to a first axis due to a Coriolis force, the second axis being situated perpendicularly to the first axis, the first and second axis being situated in parallel to the main plane of extension, the first and second drive elements being mechanically coupled to each other via a drive coupling element.