Abstract: A method for controlling traction of a wheeled vehicle or a vehicle combination having a tractor vehicle and at least one trailer vehicle. A sensor device on a coupling element of a trailer device transmits coupling forces in x, y, and z directions to the coupling element of the tractor vehicle, which are measured and emitted as force signals. From these force signals, an evaluation unit determines the coupling force acting in the respective vehicle direction and transmits them to a control unit. Traction of the tractor vehicle is adapted to suit the properties of the ground surface. Using sequences of the coupling forces, the dynamic fraction if filtered out and from these a characteristic value is determined and transmitted to the control unit. If the characteristic value exceeds a limit value, then at least one measure to improve the traction of the tractor vehicle is carried out.

Abstract: An electrical resistor has a resistance conductor, which is applied to a carrier layer, and two connection elements, which are electrically conductively connected to the resistance conductor. The two connection elements are configured to each be welded or soldered to an electrical contact in order to electrically contact the resistor. The resistance conductor for each connection element has a region that overlaps the corresponding connection element. The overlap region is in electrical contact with the corresponding connection element.

Abstract: An electrical resistor has a resistance conductor, which is applied to a carrier layer, and two connection elements, which are electrically conductively connected to the resistance conductor. The two connection elements are configured to each be welded or soldered to an electrical contact in order to electrically contact the resistor. The resistance conductor for each connection element has a region that overlaps the corresponding connection element. The overlap region is in electrical contact with the corresponding connection element.

Abstract: Satellite solar generator wing including solar panels having at least two fixed solar panels and at least one semi-fixed solar panel. The solar panels are connected to one another in order to assume an operating position and a transport position, and, in the transport position, the solar panels are retained on top of one another and the semi-fixed solar panel is arranged in a freely oscillating manner between the two fixed solar panels.

Abstract: Satellite solar generator wing including solar panels having at least two fixed solar panels and at least one semi-fixed solar panel. The solar panels are connected to one another in order to assume an operating position and a transport position, and, in the transport position, the solar panels are retained on top of one another and the semi-fixed solar panel is arranged in a freely oscillating manner between the two fixed solar panels.