Abstract: Method for operating a display device driven by at least one stepping motor with display scales, having the following steps: determining suitable step widths at least in ranges affected by stroboscopic flicker effects when driving in each case one stepping motor for moving the display scale in a measuring run when starting the instrument or on request, storing the determined step widths in the form of a matching parameter, and operating the stepping motor(s) with a suitable step-width resolution in the ranges that are identified as affected by the stroboscopic flicker effects to be avoided.

Abstract: Method for operating a display device driven by at least one stepping motor with display scales, having the following steps: determining suitable step widths at least in ranges affected by stroboscopic flicker effects when driving in each case one stepping motor for moving the display scale in a measuring run when starting the instrument or on request, storing the determined step widths in the form of a matching parameter, and operating the stepping motor(s) with a suitable step-width resolution in the ranges that are identified as affected by the stroboscopic flicker effects to be avoided.

Abstract: The invention concerns a compass having an electro magnetic half-shell transformer energy transmission and opto electronic data transmission. To avoid a slipring connection during the transfer of supply voltage at least one winding on the primary half-shell is connected to a controllable input voltage source via a H-bridge circuit, and at least one secondary winding having taps is provided at the other half-shell coil.

Abstract: The invention concerns a compass having an electro magnetic half-shell transformer energy transmission and opto electronic data transmission.

Abstract: An angle detection device with a data transmission path on an n·360° bearing assembly with at least one scanning disk (21) arranged on one of two components at right angles to the axis of rotation, and with electro-optical illumination and detection means on the respective components held together by the bearing assembly, for scanning the instantaneous angle of the scanning disk (21), wherein electro-optical data transmission means are provided on said scanning disk (21) and on a surface opposite said scanning disk (21).

Abstract: An angle detection device with a data transmission path on an n·360° bearing assembly with at least one scanning disk (21) arranged on one of two components at right angles to the axis of rotation, and with electro-optical illumination and detection means on the respective components held together by the bearing assembly, for scanning the instantaneous angle of the scanning disk (21), wherein electro-optical data transmission means are provided on said scanning disk (21) and on a surface opposite said scanning disk (21).

Abstract: The invention refers to a process for scanning a gyroscopic instrument. The invention is characterised by the collection of gyroscopic data being effected by true angle scanning. In order to apply the process of the invention, a gyroscopic instrument including a gyroscopic scanning system is required in which the gyroscopic scanning system is coupled with a rotating, scanned and/or scanning unit. The process may also refer to a gyroscopic instrument including a gyroscopic scanning system in which a scanning module (such as a CCD sensor) is arranged on the side of the gyroscopic instrument as a scanning device, directly scanning horizontal and vertical true angle identifications on a gyroscopic instrument.

Abstract: Signals from a rudder position setting control and from a rudder position sensor constitute the only electrical information sources needed for operating a monitoring system for a rudder control that produces an alarm when the rudder control does not function effectively. The difference between the desired rudder setting and the actual rudder position, generated by a differential amplifier, is fed to a bi-directional limit circuit and a differentiating circuit is used to generate a signal corresponding to the rate of change of rudder position, which signal is likewise provided to a bi-directional limit circuit.