Abstract: The disclosure is directed to an encoder apparatus that is capable of resolving magnetically axial and/or rotational displacements of a knob shaft thereof independently and includes a magnetic snap action switch, and a method of assembling the same. In one embodiment, the encoder apparatus has application as a display controller. In another embodiment, one or more of the encoder assemblies may be integrated into a bezel of a display for controlling the operations thereof.

Abstract: Multifunctional encoder apparatus comprises: a housing including a cavity and an opening extending from the cavity to the top of the housing: a knob shaft including an upper portion disposed through the housing opening, and a lower portion disposed in the cavity and including a permanent magnet magnetized with at least one set of North-South magnetic poles, the knob shaft and its permanent magnet being axially and rotatably movable in the housing cavity; a plurality of magnetic field sensors disposed within the housing cavity in proximity to the permanent magnet and distributed angularly thereabout to sense the magnetic field strength of the permanent magnet based on the orientation of the permanent magnet with respect to the sensors, each sensor for generating a signal representative of the magnitude of the magnetic field strength sensed thereby; and a processor for processing the sensor signals to independently resolve axial and rotational movement of the knob shaft.

Abstract: In accordance with the disclosed method, an attitude determining device which is installed onboard a mobile craft, like an aircraft, for example, at an unknown orientation with respect to the reference coordinate system of the craft senses its installation orientation with respect to an earth frame coordinate system when the craft is at rest to obtain a static orientation measurement thereof. Thereafter, an attitude of the mobile craft with respect to the earth frame is measured with the attitude determining device and such measurement is compensated with the static orientation measurement to obtain attitude information of the craft's reference coordinate system with respect to the earth frame coordinate system. The installation orientation of the attitude determining device may be sensed while the craft is at rest in either a leveled or unleveled condition.