Aircraft multi-mode switching method for full life cycle and related equipment thereof

According to the aircraft multi-mode switching method for the whole life cycle and the related equipment thereof, the ground control system is initialized, and the remote interaction computer of the ground control system is used for receiving the upper layer switching instruction; after an upper layer switching instruction is received, whether the aircraft launching preparation time is within a preset time range or not is judged; when the aircraft launching preparation time is not within the preset time range, controlling a remote interaction computer to be in a standby or dormant state by using an energy management and control module DPM until the aircraft launching preparation time is within the preset time range; when the aircraft launching preparation time is within a preset time range, responding to an upper layer switching instruction; equipment in the ground control system is controlled to execute a specific mode management scheme according to the upper layer switching instruction, and multi-mode auton