| 摘要 |
<p>The main subject of the present invention is an intelligent missile (1), which comprises a set of aerodynamic surfaces (2a, 2b, 2c) which can be directionally adjusted by actuating means (3a, 3b, 3c); a navigation means (7a, 7b), which determines the instantaneous position of the intelligent missile (1); an image acquisition means (10), which continuously acquires images of the space situated facing the intelligent missile (1); a communication means (13a, 13b), which receives information regarding the atmospheric conditions and the position of a target of the intelligent missile (1); and a processing means (4a, 4b) which is connected to the navigation means (7a, 7b), to the image acquisition means (10) and to the communication means (13a, 13b) and which determines, depending on the information received by said means, the instantaneous orientation of each aerodynamic surface (2a, 2b, 2c) so that the intelligent missile (1) reaches the target.</p> |
