| 摘要 |
An article of ammunition which is controllable during its final flight phase, which is equipped in its cross-sectional plane through the center of gravity with a radially oriented impulse system which is rotatable about the longitudinal axis of the article of ammunition; article, which is activatable through a control circuit located on board of the ammunition article, upon the detection of a target object which is located on the opposite side relative to the instantaneous orientation of the impulse system through the intermediary of a sensor device. Also disclosed is a method for navigating an article of ammunition which is controllable during its final flight phase towards the target object.
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