The present disclosure relates to a control system (200), to a vehicle (1), to a method (400), and to computer software (208). The method (400) is a method of controlling a user interface of a vehicle (1). The method (400) comprises obtaining (402) context information associated with use of the vehicle. The method (400) comprises providing (402) the context information to a dynamic decision model to determine (404) a display location at which to display a user interface item (502-518) on at least one of a plurality of driver-viewable displays (216, 218, 220) at different locations relative to a front windscreen (2) of the vehicle. The method (400) comprises causing (406) the user interface item (502-518) to be displayed at the determined display location. The method (400) comprises updating (410, 412, 414) the dynamic decision model in dependence on the context information and a determined user response to the display location of display of the user interface item (502-518).

A vehicle information display system an operation section provided at one side in a vehicle width direction relative to a driver seat, the operation section being structured so as to be operable by a vehicle occupant; and a display section provided at a position that is viewable from the driver seat, a vicinity information display region in which vicinity information of the vehicle being displayed being specified at a central portion of the display section, and a selection option display region being specified at one side in the vehicle width direction of the display section, relative to the vicinity information display region, the selection option display region being selectable by the vehicle occupant operating the operation section.

A system comprising a first display and a second display configured to display first and second content, respectively. The system further comprises an avionics computer configured to: process a fault status signal received from the first display; and in response, set an automatic reversion signal to a ground state, wherein setting the automatic reversion signal to the ground state causes the first display to transition away from an on state and instruct the second display to display at least in part the first content. The system further comprises a diode. The system further comprises a display controller comprising a first terminal, a second terminal, and a third terminal, wherein the first and second terminals are coupled to a first end of the diode, and wherein the third terminal is coupled to a second end of the diode and the avionics computer.