Flight control method and system of aircraft and aircraft accelerator platform

The invention discloses a flight control method and system of an aircraft and an aircraft accelerator platform. The flight control method of the aircraft comprises the steps that the real-time position of a throttle lever on an active accelerator platform is obtained; judging whether the throttle lever exceeds an automatic working area of an active throttle table or not according to the real-time position; if yes, the stroke of the throttle lever exceeding the automatic working area is obtained; judging whether the travel reaches a preset TOGA * position or not; and if the TOGA * position is reached, activating a re-flight mode, otherwise, keeping the rotating speed and the thrust of the TOGA gear unchanged. According to the technical scheme, the technical problems that in the prior art, in the key stage of re-flight of an airplane, the operation burden and the mistaken touch risk of a pilot are increased, the step that the pilot needs to operate a throttle lever is increased, certain safety risks exist, and