Method for controlling a guided missile powered by an engine

摘要

The method involves calculating a trajectory property of a trajectory (4) to a destination point (8) by a processing unit of a guided missile (2) during flying operation. The flying operation of the guided missile is controlled depending on a flight path property. The flying speed of the guided missile is influenced during the calculation of the flight path property, and a steering-free flow process is controllably provided by the processing unit. The flying of the guided missile is controlled depending on a position of a false point relative to destination point. An independent claim is also included for a guided missile comprising a drive device.