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Cruise missile and methods of controlling a cruise missile
Cruise missile and methods of controlling a cruise missile
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机译：巡航导弹和控制巡航导弹的方法
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摘要
A cruise missile comprises a fuselage body defining a missile longitudinal axis, which forms an interior space, a fuel tank arranged in the interior space for holding liquid fuel, an engine arranged at a rear end of the fuselage body, a fuel pump for conveying liquid fuel from the fuel tank into the engine, at least two control fins arranged in the area of the rear end of the fuselage body, at least two wings, an actuator system kinematically coupled to the wings for moving the wings relative to the fuselage body in such a way that an angle of sweep of the wings can be varied, and a control device. This is set up to provide pump control signals for controlling a fuel delivery rate of the fuel pump, to determine a current fuel mass in the fuel tank based on the pump control signals, to determine a current position of a center of gravity of the cruise missile in relation to the missile longitudinal axis based on the determined current fuel mass and to determine actuator control signals for actuation of the actuator system in order to set a current position of an aerodynamic pressure point of the cruise missile in relation to the missile longitudinal axis depending on the current position of the center of mass.
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