Abstract:
A LIDAR system including a light source for emitting a light pulse along an optical axis, a deflection device to deflect in an oscillating manner the light pulse along the optical axis in first and second spatial directions so that the light pulse along the optical axis repeatedly runs through a two-dimensional scan pattern, and a control unit for activating and deactivating the light source. The oscillating deflection in the first spatial direction is achieved by repeated first partial movements and second partial movements. The oscillating deflection in the second spatial direction is achieved by repeated third partial movements and fourth partial movements. The control unit activates the light source to emit a light pulse at predefined locations of the scan pattern, and activates the light source to emit a light pulse at different pixels during the first partial movements and/or third partial movements than during the second partial movements and/or fourth partial movements.
Abstract:
A system having an inertial sensor and an evaluation unit. The inertial sensor is configured to excite an oscillatory structure of the inertial sensor to execute a drive oscillation, so that an output data rate of the inertial sensor is derived as a function of a frequency of the drive oscillation. The evaluation unit has a reference clock generator and is configured to ascertain the output data rate of the inertial sensor as a function of a reference frequency of the reference clock generator and to determine the frequency and/or frequency change of the drive oscillation as a function of the ascertained output data rate. Alternatively, the inertial sensor is configured to receive a reference clock signal of the reference clock generator from the evaluation unit and to determine the frequency and/or frequency change as a function of the transmitted reference clock signal.
Abstract:
A LIDAR system that includes a laser unit, a receiving unit, and a cooling device for generating a cooling airflow. The laser unit, the receiving unit, and the cooling device are situated rotatingly about a rotational axis, so that the cooling airflow for cooling the rotating components is generated by the LIDAR system itself.
Abstract:
A micromechanical rate-of-rotation sensor includes a first Coriolis element. The micromechanical rate-of-rotation sensor further includes a first drive beam arranged along the first Coriolis element. The first drive beam is coupled via a first spring to the first Coriolis element. The micromechanical rate-of-rotation sensor further includes a first drive electrode carrier extending from the first drive beam in a direction opposite to the first Coriolis element. The first drive electrode carrier is configured to carry a multiplicity of first drive electrodes extending parallel to the first drive beam.
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 including a substrate having a main plane of extension, a first rotation rate sensor structure for detecting a first rotation rate about an axis that is in parallel to a first axis extending in parallel to the main plane of extension, and a second rotation rate sensor structure for detecting a second rotation rate about an axis that is parallel to a second axis extending perpendicularly with respect to the main plane of extension. Also included is drive device for deflecting a first structure of the first rotation rate sensor structure, and a second structure of the first rotation rate sensor structure, and also for deflecting a third structure of the second rotation rate sensor structure, and a fourth structure of the second rotation rate sensor structure, in such a way that the first, second, third, and fourth structures are excitable into a mechanically coupled oscillation.
Abstract:
A sensor drive includes at least one first seismic mass and an operating apparatus. The operating apparatus is configured to put the first seismic mass into oscillatory motion such that (i) a projection of the oscillatory motion of the first seismic mass onto a first spatial direction is a first harmonic oscillation of the first seismic mass at a first frequency, and (ii) a projection of the oscillatory motion of the first seismic mass onto a second spatial direction oriented at an angle to the first spatial direction is a second harmonic oscillation of the first seismic mass at a second frequency not equal to the first frequency. A method includes operating such a sensor device having at least one seismic mass.
Abstract:
A micromechanical spring for an inertial sensor, including segments of a monocrystalline base material, the segments having surfaces which are situated at a right angle to one another with respect to a plane of oscillation of the spring and normal to the plane of oscillation of the spring, the segments being manufactured in a crystal-direction-dependent etching process and each having two different orientations normal to the plane of oscillation, in which the spring includes a defined number of segments situated in a defined manner.
Abstract:
A production process for a micromechanical component includes at least partially structuring at least one structure from at least one monocrystalline silicon layer by at least performing a crystal-orientation-dependent etching step on an upper side of the silicon layer with a given (110) surface orientation of the silicon layer. For the at least partial structuring of the at least one structure, at least one crystal-orientation-independent etching step is additionally performed on the upper side of the silicon layer with the given (110) surface orientation of the silicon layer.