| 摘要 |
<p>The invention concerns in particular the field of devices for guiding or piloting of projectiles self-propelled or not or missiles (1) and concerns a method, and an associated device, for piloting a hyper-fast projectile, such as, for example, a shell, a bullet or a missile (1), comprising a globally conical nose (4), having a more or less pointed end. Said method is characterized in that it consists in performing a plasma discharge (6) in the vicinity of said end and on a limited region of the outer surface of the nose (4).</p> |
