A magnetic sensor system includes a magnetic field generator and a magnetic sensor. The magnetic sensor includes a plurality of MR elements. The plurality of MR elements are each configured so that a bias magnetic field in a second direction orthogonal to a first direction is applied to a free layer, and to change in resistance with a strength of a magnetic field component. A maximum strength of the magnetic field component applied to each of the MR elements is greater than or equal to 1.2 times the strength of a bias magnetic field.

A magnetic-field-based angle sensor system includes a stator component and a rotor component rotatable relative thereto, a magnetic field sensor operating in saturation operation and a magnetic field sensor operating in linear operation, wherein the magnetic field sensor operating in saturation operation is configured to determine a rotation angle of the rotor component relative to the stator component, and wherein the magnetic field sensor operating in linear operation is configured to ascertain an external magnetic stray field acting on the angle sensor system. The angle sensor system further includes a control device configured, based on the ascertained external magnetic stray field, to compensate for a stray-field-dependent measurement deviation in the determination of the rotation angle carried out.

Measuring distance along a wire rope, by steps that include moving the wire rope across a sensor head; counting rotations of a rotary encoder driven by the moving wire rope; detecting a first distance marker crossing the sensor head at a first position of the wire rope; detecting a second distance marker crossing the sensor head at a second position of the wire rope; and establishing calibration parameters for producing a calibrated distance measurement corresponding to any output of the rotary encoder, based at least on correlating a known distance between the first and second distance markers to a counted number of pulses of the rotary encoder between the first and second positions of the wire rope.

A system and method for blade angle position feedback. The system comprises an annular member operatively connected to rotate with a propeller, a sensor fixedly mounted adjacent the annular member and configured for detecting a passage of each singularity as the annular member is rotated and axially displaced and for generating a sensor signal accordingly, the annular member and sensor configured for relative axial displacement between a first relative axial position and a second relative axial position respectively corresponding to the first and the second mode of operation, and a detection unit connected to the sensor for receiving the sensor signal therefrom, determining on the basis of the sensor signal a time interval elapsed between the passage of successive singularities, and computing from the time interval blade angle position.

A position encoder comprising a cylindrical rotor; first and second magnetic poles having opposite polarity helically disposed about the inner or outer diameter of the rotor; first and second Hall sensors disposed within a distance suitable for the Hall sensors to detect the magnet poles.

A system and method for providing feedback for an aircraft-bladed rotor about a longitudinal axis and having an adjustable blade pitch angle. At least one position marker is provided at the rotor, extends along an axial direction, from a first end to a second end, and has varying magnetic permeability from the first end to the second end. At least one sensor is coupled to the rotor and configured for producing, as the rotor rotates about the longitudinal axis, at least one sensor signal in response to detecting passage of the at least one position marker. A control unit is communicatively coupled to the at least one sensor and configured to generate a feedback signal indicative of the blade pitch angle in response to the at least one sensor signal received from the at least one sensor.

An interpolated position of an incremental encoder is provided. A first signal and a second signal having a quadrature relationship are received from the incremental encoder. A coarse position of the incremental encoder at a first time is produced using the quadrature relationship between the first signal and the second signal. An arcsine or arccosine value based on the first signal at the first time is determined using a lookup table and a fine position of the incremental encoder is calculated using the determined value. The interpolated position of the incremental encoder, based on both the coarse position and the fine position, is then provided.

A sensor-bearing unit providing: a bearing centered on a rotation axis; a sensor device including a differential detection cell that has a structural pitch and defines a pitch plane extending along the structural pitch and along a reading direction; and an impulse ring having a magnetic pattern that includes positive poles and negative poles separated by pattern borders and which defines a tangent plane perpendicular to the pitch plane. The sensor device and the impulse ring are configured for tracking a rotation of the bearing around the rotation axis, the differential detection cell of the sensor device reading the magnetic pattern of the impulse ring along the reading direction. Each pattern border defines a nonzero pattern angle relative to the pitch plane. The invention also concerns a mechanical system with such an impulse ring. The invention also concerns a method for manufacturing such an impulse ring.

A sensor system for detecting a characteristic of a target object is described. The sensor system can include a sensor, such as a magnetic sensor, configured to sense magnet field components and to generate corresponding magnet field component signals based on the sensed magnet field components. The sensor system can include a processor that is configured to calculate a magnetic field angle based third magnetic field components. For example, the magnetic field angle can be calculated by determining a quadratic sum of a plurality of the magnetic field components. The characteristic of the target object can be determined based on the calculated magnetic field angle.

A device includes a permanent magnetic material extending along a path, a first magnetic angle sensor configured to output at least a first signal and being positioned remotely from the material, and a second magnetic angle sensor configured to output at least one second signal and being positioned remotely from the material and from the first magnetic angle sensor. Based on the at least one first signal and the at least one second signal, a relative positioning of the first magnetic angle sensor and the second magnetic angle sensor with respect to the material in parallel to the path is determined. The magnetization of the material has a periodicity that varies along the path.