Abstract: In a method for transmitting a data element from a sensor module that produces sensor data to an application unit, the data element is stored in a ring buffer in the sensor module, and a corresponding item of event information is produced in an evaluation circuit from the sensor data, the data element including the sensor data and the item of event information, the data element being transmitted from the ring buffer to the application unit upon request by the application unit.

Abstract: In a method for determining an offset of measured values of a multiaxial directional sensor using a superposed signal, a large number of multiaxial measured values are recorded first. Measured values, which are recorded in different orientations of the directional sensor, form a geometric figure in a coordinate system resulting from the measuring axes of the sensor, the ideal form of the geometric figure being known and the ideal center point of which being located at the origin of the measuring axes. In the case of a biaxial sensor, the geometric figure is a circle; in the case of a triaxial sensor, it is a sphere around the origin. The superposition caused by the interference is reflected in that the center point of the geometric figure is shifted in relation to the origin of the measuring axes. The offset is measured by determining this shift.

Abstract: In a method for determining an idle state: acceleration values are ascertained as a function of three spatial directions; a comparison value is generated from the acceleration values for each of the three spatial directions; each of the comparison values is compared with a threshold value; an interrupt signal is generated if the comparison value is less than the threshold value for each of the three spatial directions; and an electronic component is switched from a power saving state to an operating state as a function of the interrupt signal.

Abstract: A method is provided for controlling an electric apparatus having a sensor unit, the apparatus being operated in a first potential motion mode and/or in a second potential motion mode; a sensor signal being generated in the sensor unit; the first information and/or the second information being calculated as function of the sensor signal, as a function of a requirement for providing a first information with respect to the presence of the first potential motion mode and/or a second information with respect to the presence of the second potential motion mode.

Abstract: A rotation rate sensor comprises a substrate and two structures which move relative to the substrate on a design plane (x-y), with the two moving structures being coupled to form a coupled structure such that the coupled structure has a first oscillation mode with antiphase deflections of the moving structures in a first direction (x) on the design plane (x-y) as excitation mode. The coupled structure has a second oscillation mode as a detection mode which is excited by Coriolis accelerations when the first oscillation mode is excited and on rotation about a sensitive axis (z) of the rotation rate sensor. The sensitive axis is at right angles to the design plane (x-y), and the coupled structure is designed such that, subject to optimal preconditions, it does not have any oscillation mode which can be excited by linear accelerations of the rotation rate sensor in a direction parallel to the second axis.

Abstract: A yaw rate sensor having a substrate and a seismic mass is described, in which the seismic mass is excitable to a working oscillation relative to the substrate via a drive unit, and a Coriolis deflection of the seismic mass is detectable relative to the substrate, in which the yaw rate sensor furthermore has an interrupt interface, the drive unit being configured to reduce a frequency and/or an amplitude of the working oscillation if an interrupt signal is present at the interrupt interface.

Abstract: A method for calibrating a triaxial magnetic field sensor includes steps for determining an offset of recorded measured values of the magnetic field sensor using a superposed signal and for determining the sensitivity of the magnetic field sensor along the first measuring axes. The determination of the sensitivity includes steps for determining the sensitivity of the magnetic field sensor along a first measuring axis and for determining the sensitivity of the magnetic field sensor along the other measuring axes based on the sensitivity of the first measuring axis and the determined offset.

Abstract: In a method for determining an offset of measured values of a multiaxial directional sensor using a superposed signal, a large number of multiaxial measured values are recorded first. Measured values, which are recorded in different orientations of the directional sensor, form a geometric figure in a coordinate system resulting from the measuring axes of the sensor, the ideal form of the geometric figure being known and the ideal center point of which being located at the origin of the measuring axes. In the case of a biaxial sensor, the geometric figure is a circle; in the case of a triaxial sensor, it is a sphere around the origin. The superposition caused by the interference is reflected in that the center point of the geometric figure is shifted in relation to the origin of the measuring axes. The offset is measured by determining this shift.

Abstract: In a method for determining an idle state: acceleration values are ascertained as a function of three spatial directions; a comparison value is generated from the acceleration values for each of the three spatial directions; each of the comparison values is compared with a threshold value; an interrupt signal is generated if the comparison value is less than the threshold value for each of the three spatial directions; and an electronic component is switched from a power saving state to an operating state as a function of the interrupt signal.

Abstract: A method for calibrating an acceleration sensor includes the following sequential steps: ascertaining acceleration values as a function of three spatial directions; for each of the three spatial directions, generating a comparison value from the acceleration values; comparing each of the comparison values to a first threshold value; calculating a cumulative value as a function of at least one acceleration value for each of the three spatial directions; comparing the cumulative value to a second threshold value; and calibrating the acceleration sensor when, in the third method step, for each of the three spatial directions, the comparison value is less than the threshold value, and when, in the fifth method step, the cumulative value is greater than the further threshold value.

Abstract: In a method for detecting free fall, a first acceleration parallel to a first axis, a second acceleration parallel to a second axis perpendicular to the first axis, and a third acceleration parallel to a third axis perpendicular to the first axis and to the second axis are measured. A sum of a first value of the first acceleration, a second value of the second acceleration, and a third value of the third acceleration is calculated, and the free fall is detected as a function of the sum.

Abstract: A rotation rate sensor comprises a substrate and two structures which move relative to the substrate on a design plane (x-y), with the two moving structures being coupled to form a coupled structure such that the coupled structure has a first oscillation mode with antiphase deflections of the moving structures in a first direction (x) on the design plane (x-y) as excitation mode. The coupled structure has a second oscillation mode as a detection mode which is excited by Coriolis accelerations when the first oscillation mode is excited and on rotation about a sensitive axis (z) of the rotation rate sensor. The sensitive axis is at right angles to the design plane (x-y), and the coupled structure is designed such that, subject to optimal preconditions, it does not have any oscillation mode which can be excited by linear accelerations of the rotation rate sensor in a direction parallel to the second axis.