AUTOREVERSION CIRCUIT FOR SPACECRAFT DISPLAYS PERFORMED USING HARDWARE IMPLEMENTATION

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.